Started by upstream project "ESP_RegCaps" build number 619 originally caused by: Started by an SCM change Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on macys_VM in workspace /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Done Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS/pyEGADS/__pycache__ Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/circle1_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/circle2_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/naca_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/EGADS_dot/src/ruled_naca_dot Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/UDP_UDF/data/tire Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/UDP_UDF/data/tire.o Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/UDP_UDF/data/tire.so Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/UDP_UDF/data/udpTire.o Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/Tutorial/egads2tri Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/Tutorial/egads2tri.o Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/Tutorial/tire Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/Tutorial/tire.o Updating svn+ssh://acdl.mit.edu/home/svnroot/EGADS at revision '2024-03-05T22:19:11.419 -0500' 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 trunk/src/egadsGeom.cpp At revision 2021 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/autoLink_Pytest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/avl_AutoSpan_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/avl_ControlSurf_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/avl_DesignSweep_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/avl_EigenValue_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/avl_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/awave_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/friction_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/tsfoil_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/pyCAPS/xfoil_PyTest Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/pyCAPS/pyCAPS/__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/CAPS at revision '2024-03-05T22:19:11.419 -0500' 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 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 AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.43.31 PM.png 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 AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.45.36 PM.png AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.46.10 PM.png AU training/lectures/ParaviewBasics/Screen Shot 2019-04-26 at 12.46.34 PM.png 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 At revision 4074 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP Updating svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-03-05T22:19:11.419 -0500' 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 data/CAPS/csmOCCFailure_7.8.txt A data/TRADES/csmOCCFailure_7.8.txt A data/basic/csmOCCFailure_7.8.txt A data/capsExamples/csmOCCFailure_7.8.txt A data/csmIgnore_7.8.txt A data/csmOCCFailure_7.8.txt A data/gallery/csmOCCFailure_7.8.txt A data/legacy/csmOCCFailure_7.8.txt A data/studentGallery/csmOCCFailure_7.8.txt A data/training/csmOCCFailure_7.8.txt A data/vsp3/csmOCCFailure_7.8.txt A valgrind/valgrind-OCC7.8.supp At revision 849 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/src Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src at revision '2024-03-05T22:19:11.419 -0500' 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 2472 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/udc Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc at revision '2024-03-05T22:19:11.419 -0500' 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 2472 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/data Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-03-05T22:19:11.419 -0500' 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 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 2472 Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM Deleting /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-03-05T22:19:11.419 -0500' 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 2472 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/CAPS 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/src since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [macys_VM] is in [[macys, macys_VM, reynolds, viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN64] $ /bin/bash -xe /var/folders/qk/9zkf0syn149fvhw9mh7hgd5w0000gp/T/jenkins233569044790246974.sh + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training/lectures + [[ CAPS/LINEARAERO != *\S\l\u\g\s* ]] + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/data/Slugs + [[ macys_VM == *\v\i\g\g\e\n* ]] + bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/ESP_Regression.sh + source /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/ESP_Env.sh ++ export OCCTREF=7.6 ++ OCCTREF=7.6 ++ AFLR_VERSION=11.5.9 ++ SU2_VERSION=8.0.0 ++ TETGEN_VERSION=1.6.0 ++ VSP_VERSION=3.34.0 ++ export PYTHON_VERSION=3.11.6 ++ PYTHON_VERSION=3.11.6 ++ export EFCOMP=gfortran ++ EFCOMP=gfortran ++ [[ macys_VM == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN64 == *\.\i\f\o\r\t ]] ++ '[' -f /opt/intel/oneapi/setvars.sh ']' ++ source /opt/intel/oneapi/setvars.sh ++ '[' -f /Users/jenkins/.bashrc ']' ++ export CAPS_OUTLEVEL=0 ++ CAPS_OUTLEVEL=0 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.6 != '' ]] ++ [[ '' != '' ]] ++ [[ macys_VM == *\r\e\y\n\o\l\d\s* ]] ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile +++ [[ -r /usr/local/etc/profile.d/bash_completion.sh ]] +++ . /usr/local/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return +++ export PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin +++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.6.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/udunits/udunits2.xml ++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs ++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/lib:/opt/intel/oneapi/tbb/2021.3.0/env/../lib:/opt/intel/oneapi/mkl/2021.3.0/lib:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib/intel64_mac:/opt/intel/oneapi/compiler/2021.3.0/mac/compiler/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9 ++ [[ macys_VM == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-x86-64 ++ AFLR_ARCH=MacOSX-x86-64 ++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit ++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ++ export CART3D_ARCH=OSX64_ICC ++ CART3D_ARCH=OSX64_ICC ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS ++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.34.0-MacOS ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/ ++ [[ macys_VM == \m\a\c\y\s ]] ++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0 ++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0 ++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ macys_VM == \m\a\c\y\s* ]] ++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/intercept-*' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ ln -s /usr/local/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/python ++ ln -s /usr/local/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/python-config ++ ln -s /usr/local/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/virtualenv +++ python-config --includes ++ export 'PYTHONINC=. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' ++ PYTHONINC='. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]] +++ python-config --ldflags --embed ++ export 'PYTHONLIB=-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation' ++ [[ macys_VM == \m\a\c\y\s ]] ++ [[ macys_VM == \v\i\g\g\e\n ]] ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.5 ++ [[ DARWIN64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/data + source /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/ESPbfr.sh ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ ++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/ESPbfr.tgz x ESP/ x ESP/CYGWIN64/ x ESP/CYGWIN64/bin/ x ESP/CYGWIN64/bin/mastros.exe x ESP/CYGWIN64/bin/ASTRO.D01 x ESP/CYGWIN64/bin/ASTRO.IDX x ESP/CYGWIN64/include/ x ESP/CYGWIN64/lib/ x ESP/CYGWIN64/lib/libquadmath-0.dll x ESP/CYGWIN64/lib/libwinpthread-1.dll x ESP/CYGWIN64/lib/libgcc_s_sjlj-1.dll x ESP/CYGWIN64/obj/ x ESP/CYGWIN64/test/ x ESP/DARWIN64/ x ESP/DARWIN64/bin/ x ESP/DARWIN64/bin/mastros.exe x ESP/DARWIN64/bin/ASTRO.D01 x ESP/DARWIN64/bin/mset x ESP/DARWIN64/bin/ASTRO.IDX x ESP/DARWIN64/bin/avl x ESP/DARWIN64/bin/xfoil x ESP/DARWIN64/bin/mses x ESP/DARWIN64/include/ x ESP/DARWIN64/include/nmb.h x ESP/DARWIN64/include/xddm/ x ESP/DARWIN64/include/xddm/xddmInternals.h x ESP/DARWIN64/include/xddm/xddm.h x ESP/DARWIN64/include/xddm/xddm.c x ESP/DARWIN64/include/converter.h x ESP/DARWIN64/include/libCart3D/ x ESP/DARWIN64/include/libCart3D/sensors.h x ESP/DARWIN64/include/libCart3D/SFC.h x ESP/DARWIN64/include/libCart3D/map.h x ESP/DARWIN64/include/libCart3D/MGinfo.h x ESP/DARWIN64/include/libCart3D/gridStructures.h x ESP/DARWIN64/include/libCart3D/timer.h x ESP/DARWIN64/include/libCart3D/ConvInfo.h x ESP/DARWIN64/include/libCart3D/dualtime.h x ESP/DARWIN64/include/libCart3D/stateVector.h x ESP/DARWIN64/include/libCart3D/cartCells.h x ESP/DARWIN64/include/libCart3D/encoding.h x ESP/DARWIN64/include/libCart3D/string_util.h x ESP/DARWIN64/include/libCart3D/int64.h x ESP/DARWIN64/include/libCart3D/bBox_stuff.h x ESP/DARWIN64/include/libCart3D/basicTypes.h x ESP/DARWIN64/include/libCart3D/utils_xml.h x ESP/DARWIN64/include/libCart3D/hex.h x ESP/DARWIN64/include/libCart3D/PostProcInfo.h x ESP/DARWIN64/include/libCart3D/SolverInfo.h x ESP/DARWIN64/include/libCart3D/earthBL_BC.h x ESP/DARWIN64/include/libCart3D/limiters.h x ESP/DARWIN64/include/libCart3D/geomStructures.h x ESP/DARWIN64/include/libCart3D/CaseInfo.h x ESP/DARWIN64/include/libCart3D/memory_util.h x ESP/DARWIN64/include/libCart3D/infoStructures.h x ESP/DARWIN64/include/libCart3D/geomTypes.h x ESP/DARWIN64/include/libCart3D/c3d_timeout.h x ESP/DARWIN64/include/libCart3D/myLList.h x ESP/DARWIN64/include/libCart3D/IOinfo.h x ESP/DARWIN64/include/libCart3D/GridInfo.h x ESP/DARWIN64/include/libCart3D/c3d_global.h x ESP/DARWIN64/include/libCart3D/vortexBC.h x ESP/DARWIN64/include/c3dio/ x ESP/DARWIN64/include/c3dio/c3dio_icemcfd.h x ESP/DARWIN64/include/c3dio/c3dio_lib.h x ESP/DARWIN64/include/udunits.h x ESP/DARWIN64/include/udunits2.h x ESP/DARWIN64/lib/ x ESP/DARWIN64/lib/libudunits2.dylib x ESP/DARWIN64/lib/libudunits2.0.dylib x ESP/DARWIN64/lib/libCart3D.a x ESP/DARWIN64/lib/libnmb.dylib x ESP/DARWIN64/lib/libc3dio.a x ESP/DARWIN64/obj/ x ESP/DARWIN64/test/ x ESP/DARWIN_ARM64/ x ESP/DARWIN_ARM64/bin/ x ESP/DARWIN_ARM64/bin/mastros.exe x ESP/DARWIN_ARM64/bin/ASTRO.D01 x ESP/DARWIN_ARM64/bin/mset x ESP/DARWIN_ARM64/bin/ASTRO.IDX x ESP/DARWIN_ARM64/bin/avl x ESP/DARWIN_ARM64/bin/xfoil x ESP/DARWIN_ARM64/bin/mses x ESP/DARWIN_ARM64/include/ x ESP/DARWIN_ARM64/include/nmb.h x ESP/DARWIN_ARM64/include/xddm/ x ESP/DARWIN_ARM64/include/xddm/xddmInternals.h x ESP/DARWIN_ARM64/include/xddm/xddm.h x ESP/DARWIN_ARM64/include/xddm/xddm.c x ESP/DARWIN_ARM64/include/converter.h x ESP/DARWIN_ARM64/include/libCart3D/ x ESP/DARWIN_ARM64/include/libCart3D/sensors.h x ESP/DARWIN_ARM64/include/libCart3D/SFC.h x ESP/DARWIN_ARM64/include/libCart3D/map.h x ESP/DARWIN_ARM64/include/libCart3D/MGinfo.h x ESP/DARWIN_ARM64/include/libCart3D/gridStructures.h x ESP/DARWIN_ARM64/include/libCart3D/timer.h x ESP/DARWIN_ARM64/include/libCart3D/ConvInfo.h x ESP/DARWIN_ARM64/include/libCart3D/dualtime.h x ESP/DARWIN_ARM64/include/libCart3D/stateVector.h x ESP/DARWIN_ARM64/include/libCart3D/cartCells.h x ESP/DARWIN_ARM64/include/libCart3D/encoding.h x ESP/DARWIN_ARM64/include/libCart3D/string_util.h x ESP/DARWIN_ARM64/include/libCart3D/int64.h x ESP/DARWIN_ARM64/include/libCart3D/bBox_stuff.h x ESP/DARWIN_ARM64/include/libCart3D/basicTypes.h x ESP/DARWIN_ARM64/include/libCart3D/utils_xml.h x ESP/DARWIN_ARM64/include/libCart3D/hex.h x ESP/DARWIN_ARM64/include/libCart3D/PostProcInfo.h x ESP/DARWIN_ARM64/include/libCart3D/SolverInfo.h x ESP/DARWIN_ARM64/include/libCart3D/earthBL_BC.h x ESP/DARWIN_ARM64/include/libCart3D/limiters.h x ESP/DARWIN_ARM64/include/libCart3D/geomStructures.h x ESP/DARWIN_ARM64/include/libCart3D/CaseInfo.h x ESP/DARWIN_ARM64/include/libCart3D/memory_util.h x ESP/DARWIN_ARM64/include/libCart3D/infoStructures.h x ESP/DARWIN_ARM64/include/libCart3D/geomTypes.h x ESP/DARWIN_ARM64/include/libCart3D/c3d_timeout.h x ESP/DARWIN_ARM64/include/libCart3D/myLList.h x ESP/DARWIN_ARM64/include/libCart3D/IOinfo.h x ESP/DARWIN_ARM64/include/libCart3D/GridInfo.h x ESP/DARWIN_ARM64/include/libCart3D/c3d_global.h x ESP/DARWIN_ARM64/include/libCart3D/vortexBC.h x ESP/DARWIN_ARM64/include/c3dio/ x ESP/DARWIN_ARM64/include/c3dio/c3dio_icemcfd.h x ESP/DARWIN_ARM64/include/c3dio/c3dio_lib.h x ESP/DARWIN_ARM64/include/udunits.h x ESP/DARWIN_ARM64/include/udunits2.h x ESP/DARWIN_ARM64/lib/ x ESP/DARWIN_ARM64/lib/libudunits2.dylib x ESP/DARWIN_ARM64/lib/libudunits2.0.dylib x ESP/DARWIN_ARM64/lib/libCart3D.a x ESP/DARWIN_ARM64/lib/libc3dio.a x ESP/DARWIN_ARM64/obj/ x ESP/DARWIN_ARM64/test/ x ESP/LINUX64/ x ESP/LINUX64/bin/ x ESP/LINUX64/bin/mastros.exe x ESP/LINUX64/bin/ASTRO.D01 x ESP/LINUX64/bin/mset x ESP/LINUX64/bin/ASTRO.IDX x ESP/LINUX64/bin/avl x ESP/LINUX64/bin/xfoil x ESP/LINUX64/bin/mses x ESP/LINUX64/include/ x ESP/LINUX64/include/nmb.h x ESP/LINUX64/include/xddm/ x ESP/LINUX64/include/xddm/xddmInternals.h x ESP/LINUX64/include/xddm/xddm.h x ESP/LINUX64/include/xddm/xddm.c x ESP/LINUX64/include/libCart3D/ x ESP/LINUX64/include/libCart3D/sensors.h x ESP/LINUX64/include/libCart3D/SFC.h x ESP/LINUX64/include/libCart3D/map.h x ESP/LINUX64/include/libCart3D/MGinfo.h x ESP/LINUX64/include/libCart3D/gridStructures.h x ESP/LINUX64/include/libCart3D/timer.h x ESP/LINUX64/include/libCart3D/ConvInfo.h x ESP/LINUX64/include/libCart3D/dualtime.h x ESP/LINUX64/include/libCart3D/stateVector.h x ESP/LINUX64/include/libCart3D/cartCells.h x ESP/LINUX64/include/libCart3D/encoding.h x ESP/LINUX64/include/libCart3D/string_util.h x ESP/LINUX64/include/libCart3D/int64.h x ESP/LINUX64/include/libCart3D/bBox_stuff.h x ESP/LINUX64/include/libCart3D/basicTypes.h x ESP/LINUX64/include/libCart3D/utils_xml.h x ESP/LINUX64/include/libCart3D/hex.h x ESP/LINUX64/include/libCart3D/PostProcInfo.h x ESP/LINUX64/include/libCart3D/SolverInfo.h x ESP/LINUX64/include/libCart3D/earthBL_BC.h x ESP/LINUX64/include/libCart3D/limiters.h x ESP/LINUX64/include/libCart3D/geomStructures.h x ESP/LINUX64/include/libCart3D/CaseInfo.h x ESP/LINUX64/include/libCart3D/memory_util.h x ESP/LINUX64/include/libCart3D/infoStructures.h x ESP/LINUX64/include/libCart3D/geomTypes.h x ESP/LINUX64/include/libCart3D/c3d_timeout.h x ESP/LINUX64/include/libCart3D/myLList.h x ESP/LINUX64/include/libCart3D/IOinfo.h x ESP/LINUX64/include/libCart3D/GridInfo.h x ESP/LINUX64/include/libCart3D/c3d_global.h x ESP/LINUX64/include/libCart3D/vortexBC.h x ESP/LINUX64/include/c3dio/ x ESP/LINUX64/include/c3dio/c3dio_icemcfd.h x ESP/LINUX64/include/c3dio/c3dio_lib.h x ESP/LINUX64/lib/ x ESP/LINUX64/lib/libnmb.so x ESP/LINUX64/lib/libCart3D.a x ESP/LINUX64/lib/libc3dio.a x ESP/LINUX64/obj/ x ESP/LINUX64/test/ x ESP/WIN64/ x ESP/WIN64/bin/ x ESP/WIN64/bin/mses.exe x ESP/WIN64/bin/avl.exe x ESP/WIN64/bin/mastros.exe x ESP/WIN64/bin/ASTRO.D01 x ESP/WIN64/bin/xfoil.exe x ESP/WIN64/bin/ASTRO.IDX x ESP/WIN64/bin/mset.exe x ESP/WIN64/include/ x ESP/WIN64/include/nmb.h x ESP/WIN64/include/winhelpers/ x ESP/WIN64/include/winhelpers/gettimeofday.h x ESP/WIN64/include/winhelpers/websock-w32.h x ESP/WIN64/include/winhelpers/netdb.h x ESP/WIN64/include/winhelpers/unistd.h x ESP/WIN64/include/winhelpers/strings.h x ESP/WIN64/include/winhelpers/sys/ x ESP/WIN64/include/winhelpers/sys/time.h x ESP/WIN64/include/converter.h x ESP/WIN64/include/udunits.h x ESP/WIN64/include/udunits2.h x ESP/WIN64/lib/ x ESP/WIN64/lib/libquadmath-0.dll x ESP/WIN64/lib/nmb.lib x ESP/WIN64/lib/libwinpthread-1.dll x ESP/WIN64/lib/udunits2.lib x ESP/WIN64/lib/libgcc_s_sjlj-1.dll x ESP/WIN64/lib/expat.dll x ESP/WIN64/lib/udunits2.dll x ESP/WIN64/lib/nmb.dll x ESP/WIN64/obj/ x ESP/WIN64/test/ x ESP/LINUX_AARCH64/ x ESP/LINUX_AARCH64/bin/ x ESP/LINUX_AARCH64/bin/mastros.exe x ESP/LINUX_AARCH64/bin/ASTRO.D01 x ESP/LINUX_AARCH64/bin/mset x ESP/LINUX_AARCH64/bin/ASTRO.IDX x ESP/LINUX_AARCH64/bin/avl x ESP/LINUX_AARCH64/bin/xfoil x ESP/LINUX_AARCH64/bin/mses x ESP/LINUX_AARCH64/include/ x ESP/LINUX_AARCH64/lib/ x ESP/LINUX_AARCH64/obj/ x ESP/LINUX_AARCH64/test/ x ESP/udunits/ x ESP/udunits/udunits2-accepted.xml x ESP/udunits/udunits2-base.xml x ESP/udunits/udunits2-common.xml x ESP/udunits/udunits2.xml x ESP/udunits/udunits2-derived.xml x ESP/udunits/udunits2-prefixes.xml ++ virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv created virtual environment CPython3.11.5.final.0-64 in 1092ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv, clear=False, no_vcs_ignore=False, global=False) seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/Users/jenkins/Library/Application Support/virtualenv) added seed packages: pip==24.0, setuptools==69.0.3, wheel==0.42.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator ++ . /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/activate +++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/ESP_Regression.sh ']' +++ deactivate nondestructive +++ unset -f pydoc +++ '[' -z '' ']' +++ '[' -z '' ']' +++ hash -r +++ '[' -z '' ']' +++ unset VIRTUAL_ENV +++ unset VIRTUAL_ENV_PROMPT +++ '[' '!' nondestructive = nondestructive ']' +++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv +++ '[' darwin20 = cygwin ']' +++ '[' darwin20 = msys ']' +++ export VIRTUAL_ENV +++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test:/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/usr/local/bin:/usr/local/opt/python/libexec/bin:/opt/intel/oneapi/dev-utilities/2021.3.0/bin:/opt/intel/oneapi/compiler/2021.3.0/mac/bin/intel64:/usr/bin:/bin:/usr/sbin:/sbin:/usr/local/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ '[' x '!=' x ']' ++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv +++ VIRTUAL_ENV_PROMPT=venv +++ export VIRTUAL_ENV_PROMPT +++ '[' -z '' ']' +++ '[' -z '' ']' +++ _OLD_VIRTUAL_PS1= +++ PS1='(venv) ' +++ export PS1 +++ alias pydoc +++ true +++ hash -r ++ pip_install pip ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade pip Requirement already satisfied: pip in ./ESP/venv/lib/python3.11/site-packages (24.0) ++ pip_install f90nml ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade f90nml Collecting f90nml Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB) Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB) Installing collected packages: f90nml Successfully installed f90nml-1.4.4 ++ pip_install numpy ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl.metadata (61 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_10_9_x86_64.whl (20.6 MB) Installing collected packages: numpy Successfully installed numpy-1.26.4 ++ pip_install 'scipy!=1.9.2,!=1.9.3' ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade 'scipy!=1.9.2,!=1.9.3' Collecting scipy!=1.9.2,!=1.9.3 Using cached scipy-1.12.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (60 kB) Requirement already satisfied: numpy<1.29.0,>=1.22.4 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (1.26.4) Using cached scipy-1.12.0-cp311-cp311-macosx_10_9_x86_64.whl (38.9 MB) Installing collected packages: scipy Successfully installed scipy-1.12.0 ++ pip_install openmdao ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao Collecting openmdao Using cached openmdao-3.30.0-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.2.1-py3-none-any.whl.metadata (5.2 kB) Requirement already satisfied: numpy in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.26.4) Requirement already satisfied: scipy in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.12.0) Collecting requests (from openmdao) Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB) Collecting packaging (from openmdao) Using cached packaging-23.2-py3-none-any.whl.metadata (3.2 kB) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (33 kB) Collecting idna<4,>=2.5 (from requests->openmdao) Using cached idna-3.6-py3-none-any.whl.metadata (9.9 kB) Collecting urllib3<3,>=1.21.1 (from requests->openmdao) Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB) Collecting certifi>=2017.4.17 (from requests->openmdao) Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB) Using cached networkx-3.2.1-py3-none-any.whl (1.6 MB) Using cached packaging-23.2-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-macosx_10_9_x86_64.whl (121 kB) Using cached idna-3.6-py3-none-any.whl (61 kB) Using cached urllib3-2.2.1-py3-none-any.whl (121 kB) Installing collected packages: urllib3, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.6 networkx-3.2.1 openmdao-3.30.0 packaging-23.2 requests-2.31.0 urllib3-2.2.1 ++ [[ macys_VM == *\v\i\g\g\e\n* ]] ++ pip_install cvxopt ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_10_9_x86_64.whl (13.8 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 ++ pip_install dill ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade dill Collecting dill Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB) Using cached dill-0.3.8-py3-none-any.whl (116 kB) Installing collected packages: dill Successfully installed dill-0.3.8 ++ pip_install packaging ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging Requirement already satisfied: packaging in ./ESP/venv/lib/python3.11/site-packages (23.2) ++ pip_install matplotlib ++ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.8.3-cp311-cp311-macosx_10_12_x86_64.whl.metadata (5.8 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (5.8 kB) Collecting cycler>=0.10 (from matplotlib) Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB) Collecting fonttools>=4.22.0 (from matplotlib) Using cached fonttools-4.49.0-cp311-cp311-macosx_10_9_x86_64.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl.metadata (6.4 kB) Requirement already satisfied: numpy<2,>=1.21 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) (23.2) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.2.0-cp311-cp311-macosx_10_10_x86_64.whl.metadata (9.7 kB) Collecting pyparsing>=2.3.1 (from matplotlib) Using cached pyparsing-3.1.1-py3-none-any.whl.metadata (5.1 kB) Collecting python-dateutil>=2.7 (from matplotlib) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB) Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib) Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB) Using cached matplotlib-3.8.3-cp311-cp311-macosx_10_12_x86_64.whl (7.6 MB) Using cached contourpy-1.2.0-cp311-cp311-macosx_10_9_x86_64.whl (258 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.49.0-cp311-cp311-macosx_10_9_x86_64.whl (2.3 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_10_9_x86_64.whl (68 kB) Using cached pillow-10.2.0-cp311-cp311-macosx_10_10_x86_64.whl (3.5 MB) Using cached pyparsing-3.1.1-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.0 cycler-0.12.1 fonttools-4.49.0 kiwisolver-1.4.5 matplotlib-3.8.3 pillow-10.2.0 pyparsing-3.1.1 python-dateutil-2.9.0.post0 six-1.16.0 ++ [[ /Users/jenkins/util/ESP/ExternLibs == '' ]] ++ '[' -d /Users/jenkins/util/ESP/ExternLibs ']' ++ cp /Users/jenkins/util/ESP/ExternLibs/intersectWake.so /Users/jenkins/util/ESP/ExternLibs/markWakeEdges.so /Users/jenkins/util/ESP/ExternLibs/sansLIPAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/src ++ make touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/DARWIN64 rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/DARWIN64 cp -p ../include/DARWIN64 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/DARWIN64 touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads_dot.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads_dot.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egads.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/emp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/emp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/prm.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/prm.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsserver.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsss.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/wsss.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTris.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsTris.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/Surreal/always_inline.h clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsGeom.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsGeom.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsHLevel.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsHLevel.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsTopo.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTopo.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsCopy.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsCopy.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsSpline.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSpline.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsIO.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsIO.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsSplineFit.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSplineFit.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsSkinning.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSkinning.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include \ -I. egadsTessSens.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTessSens.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 OCC/BRepLib_FuseEdges.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/BRepLib_FuseEdges.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsFit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsRobust.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSBO.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/prmCfit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/prmGrid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/prmUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsExport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSolids.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include ../util/emp.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/emp.o clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I. -I../include \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/evaluate.o clang++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I. -I../include \ ../util/rational.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/rational.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.6.0 -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/regQuads.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealD1 SurrealD1_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealD4 SurrealD4_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealS1 SurrealS1_test_suite Complete! clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SurrealS4 SurrealS4_test_suite Complete! /Library/Developer/CommandLineTools/usr/bin/make -C ../util clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 uvmap/main/uvmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmapFindUV.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmapGen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmapStructFree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmapTest.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_uvmap_Write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_add.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_bnd_adj.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_area_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_chk_edge_ratio.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_cpu_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_find_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_from_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_gen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_gen_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_ibeibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfibf.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_ibfin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_iccibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_iccin.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_idibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_inibe.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_inl_uv_bnd.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_malloc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_mben_disc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_message.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_norm_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_solve.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_struct_tasks.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_test.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_to_egads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 egadsUVmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libuvmap.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libuvmap.a clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/uvmap.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegads.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \ egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.6 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; \ ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \ evaluate.o rational.o regQuads.o; ) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsHLevel.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fgadsTopo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libfgads.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libfgads.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libfgads.a touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libemp.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libemp.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libemp.a *** EGADS Build Complete! *** ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/wvServer ++ make clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/map.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/base64-decode.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/client-handshake.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libwebsockets.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/extension-deflate-stream.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/md5.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/extension-x-google-mux.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/parsers.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/extension.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sha-1.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/server.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/wv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/browserMessage.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fwv.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/servertest.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; clang++ -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libwsserver.dylib \ base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \ -install_name '@rpath/libwsserver.dylib' \ -compatibility_version 7.6 \ -current_version 1.0.25 ) ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/lite ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteMemory.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteGeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteTopo.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteAttrs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteImport.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteString.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteTris.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I. -I../src \ ../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteTessInp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/evaLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE ../util/rational.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ratLite.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteRegQuads.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteEffect.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/liteUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslite.dylib \ liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \ egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \ liteEffect.o liteUVmap.o \ -install_name '@rpath/libegadslite.dylib' \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \ liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \ emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \ liteUVmap.o ; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libegadslitestatic.a ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/test +++ ls BSplineIGES.make CSys.make GBO.make SBO.make addKnots.make agglom.make approx.make blend.make chamfer.make closure.make edge2WB.make edges.make effective.make egads2cart.make egads2ply.make egadsGeom_dot.make egadsHLevel_dot.make egadsSpline_dot.make egadsTopo_dot.make exportLite.make extrot.make fillet.make fit.make fitTri.make fullAttr.make fuseSheets.make globalTess.make hollow.make hollowFace.make intersect.make makeCone.make makeFace3D.make makeLoop.make mapTess.make mofb.make mssb.make multiContext.make offset.make rebuild.make refObj.make replace.make revolve.make ruled.make saveTess.make scribe.make sew.make simplePer.make smallEdges.make step.make sweep.make test.make tolerance.make union.make vAttr.make vCurvature.make vEffect.make vEto.make vFrame.make vGeom.make vQuad.make vTess.make vTessInp.make xform.make ++ for file in '`ls *.make`' ++ make -f BSplineIGES.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include BSplineIGES.c -o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f CSys.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/CSys.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f GBO.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/GBO.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f SBO.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SBO.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f addKnots.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/addKnots.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f agglom.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/agglom.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -legads -lm ++ for file in '`ls *.make`' ++ make -f approx.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/approx.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f blend.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/blend.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f chamfer.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/chamfer.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f closure.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/closure.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f edge2WB.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/edge2WB.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f edges.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/edges.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f effective.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include effective.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/effective.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2cart.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egads2cart.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads2cart.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2ply.make clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. egads2ply.cpp -std=c++11 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads2ply.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I. tinyply.cpp -std=c++11 -w \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tinyply.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tinyply.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsGeom_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsHLevel_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsSpline_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsTopo_dot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f exportLite.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../util/uvmap \ ../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/exportLite.o -DSTANDALONE clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/exportLite.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f extrot.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/extrot.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fillet.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fillet.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fit.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fit.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fitTri.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fitTri.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fullAttr.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fullAttr.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fuseSheets.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f globalTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/globalTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollow.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hollow.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollowFace.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hollowFace.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f intersect.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/intersect.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeCone.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeCone.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeFace3D.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include makeFace3D.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeLoop.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeLoop.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mapTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mapTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mofb.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mofb.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mssb.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mssb.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f multiContext.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include multiContext.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/multiContext.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f offset.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/offset.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f rebuild.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/rebuild.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f refObj.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/refObj.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f replace.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/replace.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f revolve.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/revolve.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f ruled.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ruled.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f saveTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include saveTess.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/saveTess.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f scribe.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/scribe.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f sew.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sew.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f simplePer.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include simplePer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/simplePer.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f smallEdges.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include smallEdges.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/smallEdges.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/smallEdges.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f step.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/step.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f sweep.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sweep.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f test.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testc.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testf.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/parsec.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/parsef.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f tolerance.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tolerance.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f union.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/union.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w ++ for file in '`ls *.make`' ++ make -f vAttr.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vAttr.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vAttr.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vCurvature.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vCurvature.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vCurvature.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vEffect.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vEffect.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vEffect.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vEto.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vEto.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vFrame.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vFrame.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vGeom.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vGeom.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vQuad.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vQuad.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vTess.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vTess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include ../util/retessFaces.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/retessFaces.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f vTessInp.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vTessInp.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vTessInp.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ for file in '`ls *.make`' ++ make -f xform.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xform.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/Tutorial ++ make -f tire.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include tire.c clang++ -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ make -f egads2tri.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include egads2tri.c clang++ -g -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/EGADS_dot/src ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pingBodies.o clang -g -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o clang -g -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/naca_dot.o clang -g -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o clang -g -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/src ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/serveCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udp.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tim.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/serveESP.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sensCSM.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBezier.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bezier.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bezier.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/biconvex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/biconvex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/box.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/box.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBspline.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bspline.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bspline.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/catmull.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/catmull.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCompare.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/compare.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/compare.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createBEM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createBEM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createPoly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createPoly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpCsm.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/csm.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/csm.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/deform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/deform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDroop.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/droop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/droop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/editAttr.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/editAttr.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ellipse.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ellipse.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/eqn2body.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/fitcurve.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfFlend.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flend.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flend.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/freeform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/freeform.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfGanged.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ganged.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ganged.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfGuide.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/guide.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/guide.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpHex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hex.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpImport.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/import.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/import.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/kulfan.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/kulfan.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/linalg.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/linalg.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/matchBodys.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mechanism.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mechanism.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNaca.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca6mc.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nacelle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nacelle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nurbbody.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nuscale.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nuscale.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfOffset.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/offset.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/offset.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parabaloid.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpParsec.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parsec.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parsec.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpPod.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pod.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pod.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpPoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/poly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/poly.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBbox.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBbox.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBrep.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBrep.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printEgo.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printEgo.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpProp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/prop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/prop.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/radwaf.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/radwaf.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSample.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sample.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sample.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSew.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sew.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sew.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfShadow.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/shadow.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/shadow.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfSlices.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slices.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slices.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpStag.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stag.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stag.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stiffener.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stiffener.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSupell.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/supell.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/supell.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfTester1.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester1.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester1.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpTester2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vsp3.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vsp3.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/waffle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/waffle.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpWarp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/warp.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/warp.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/PDT2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/PDT2.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca456.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads -lm -Wl,-w clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timEreped.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ereped.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ereped.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timMitten.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mitten.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mitten.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPlotter.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plotter.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plotter.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timSlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slugs.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vspSetup.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/common.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/common.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/esp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/esp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/tim.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/tim.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egg.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/egg.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/udpUtilities.c ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/EGADS/trunk/docs/UDP_UDF/data ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include udpTire.c -o tire.o clang -g -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include udpTire.c touch tire.so rm tire.so clang -g -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib ++ [[ '' == '' ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS ++ make (cd src; make) touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/caps.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/caps.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/capsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimUtil.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimUtil.h touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimMesh.h rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aimMesh.h clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../include \ aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimMesh.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimMesh.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libaimUtil.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsBase.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsAnalysis.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsApprox.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsAttr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsBound.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsProblem.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsValue.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsUnits.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/conjGrad.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsFunIDs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/capsChkInpt.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. \ -I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/printObject.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; clang -g -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -ludunits2 -locsm -legads -ldl \ -install_name '@rpath/libcaps.dylib' \ -compatibility_version 1.0.25 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libcapsstatic.a clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include testingAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testingAIM.o rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingAIM.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testingAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include testingWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testingWriter.o rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingWriter.so] Error 1 (ignored) clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/testingWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include phaseUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/phaseUtil.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd aim; make) (cd utils; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/attrUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/meshUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cfdUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/miscUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/feaUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vlmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/nastranUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tecplotUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/arrayUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/deprecateUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cardUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/nastranCards.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/jsonUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/nastranOP2Reader.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libutils.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libutils.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libutils.a /Library/Developer/CommandLineTools/usr/bin/ranlib: file: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libutils.a(attrUtils.o) has no symbols mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/aim/utils/vlmUtils.h (cd avl; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/avlAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd cbaero; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o clang -g -bundle /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl (cd delaundo; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils delaundoAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd egadsTess; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils egadsTessAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd friction; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils frictionAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/frictionAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/friction.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/friction.o -Wl,-w -static-libgfortran -static-libgcc (cd fun3d; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o Building FUN3D with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dUtils.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -lm -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin (cd abaqus; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DHAVE_PYTHON -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -lm -ldl -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin (cd mystran; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils mystranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils mystranUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation (cd masstran; make) clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils masstranAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/masstranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd nastran; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils nastranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/nastranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation (cd astros; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils astrosAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils astrosUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils astrosCards.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosCards.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/astrosCards.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation (cd hsm; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils hsmAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils hsmUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils hsmAdj.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.6 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/rcm.o clang++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 rcm/genrcmi.cpp -DREVISION=7.6 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/genrcmi.o /Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/atanc.o /Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/bmdump.o /Library/Developer/CommandLineTools/usr/bin/make -C src cross.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cross.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmabd.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmbb2.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmbc.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmdep.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmeqn.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmgeo.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmglr.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmout.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmprj.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmre1.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmren.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmrfm.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmrun.o /Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmsol.o /Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ludcmp.o /Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libhsm.a rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libhsm.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/hsmAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmAdj.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/genrcmi.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -Wl,-w (cd skeleton; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils skeletonAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd su2; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2Utils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2Utils.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2_4_Cardinal.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2_5_Raven.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2_6_Falcon.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2_7_Blackbird.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils su2_8_Harrier.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_8_Harrier.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2_8_Harrier.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd tacs; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils tacsAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tacsAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation (cd tsfoil; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd xfoil; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils \ xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd mses; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesUtils.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd interference; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include interferenceAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. cloudFns.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cloudFns.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/interferenceAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd aflr2; make) clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src aflr2_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib -laflr2c -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2_version /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2_version clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib \ -laflr2c -legen -lrec2 -ldftr2 -ldftr3 -ldgeom -lotb -lqtb -lug_io -lug_cpp -lice2 -lug3 -lug2 -lug_gq -lug -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -lm (cd aflr3; make) clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src aflr3_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib -laflr3 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3_version /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3_version 16.32.49 clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/EG_getEffBodyTopos.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_check_tess_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_check_tess_ordering.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_get_bedge_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_get_edge_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_get_faceOrder.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_get_face_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_get_surf_grid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_create_tess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_tess_to_dgeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_aflr4_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_auto_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_add_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_add_ff.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_add_ret_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_bodyFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_check_bc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_data_cleanup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_edgeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_edgeFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_edit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_faceEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_faceFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_faceFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_faceLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_file_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_file_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_idef2idef.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_loopEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_nodeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_reset_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_write_topo_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_curv_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_edge_arclen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_norm_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_uv_at_t.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_uv_at_xyz.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_uv_bounds.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_xyz_at_u.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_eval_xyz_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_face_node_map.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_cad_geom_faceMatch.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_data.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src /Users/jenkins/util/AFLR/aflr_lib_11.5.9/src/egads_aflr4/egads_mzone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib \ -laflr3 -laflr43 -laflr4 -lsurf_auto_cpp -lsurf_auto -lrec3 -lug_mp -lanbl3 -laflr2c -lrec2 -lbl1 -lotb -legen -lice2 -lice3 -ldftr2 -ldftr3 -ldgeom -lug_io -lug_gq -lug_cpp -lcgns -lqtb -lug3 -lug -lug2 -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -lm (cd aflr4; make) clang -g -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src aflr4_version.c \ -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib -laflr4 -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4_version /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4_version clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src -I../utils aflr4AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-x86-64/lib \ -laflr4 -laflr2c -lsurf_auto -lsurf_auto_cpp -laflr3 -legen -lrec2 -lrec3 -ldftr3 -ldftr2 -ldgeom -lotb -lqtb -lice2 -lice3 -lug3 -lug2 -lug -lug_mp -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lc++ -lm (cd awave; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils awaveAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awaveAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm gfortran -g -c -O -frecursive -fcray-pointer -std=legacy awavemod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awave.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awave.o -Wl,-w (cd tetgen; make) clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils tetgenAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgen.o clang++ -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/predicates.o clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgenAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/tetgen.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd cart3d; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \ cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/libCart3D -I./xddm \ writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/writeTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/libCart3D \ surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/surfTrix.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xddm.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/bodyTess.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cart3dAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/ \ -lc3dio -lCart3D -ldl -lxml2 -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include cart3dTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/cart3dTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/writeTrix.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lxml2 -lm (cd pointwise; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils pointwiseAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils hashElement.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hashElement.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hashElement.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -lpthread (cd refine; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../utils -I../meshWriter/libMeshbWriter refineAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/refineAIM.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include \ -I../meshWriter/libMeshbWriter/libMeshb/sources \ ../meshWriter/libMeshbWriter/libMeshb/sources/libmeshb7.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/refineAIM.so clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd meshWriter; make) /Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter make[3]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C fastWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fastWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fastWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fastWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libMeshbWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include libMeshbWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libMeshbWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/libMeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libMeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include su2Writer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2Writer.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/su2Writer.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include ugridWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o clang -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/ugridWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm (cd custom; make) make[2]: Nothing to be done for `default'. (cd Slugs/src; make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Slugs.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. Fitter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Fitter.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. RedBlackTree.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. Tessellate.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Tessellate.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/RedBlackTree.o \ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/TestFit.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -legads \ -lpthread -lz -lm (cd test; make -f aim.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aim.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/testingAIM.csm (cd test; make -f autoExec.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/autoExec.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm \ -legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lz -lm -ldl (cd test; make -f newPhase.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/newPhase.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib \ -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (cd test; make -f basic.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/basic.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (cd test; make -f geomIn.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/geomIn.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (cd test; make -f utilsTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -ludunits2 -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -ludunits2 -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lutils -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -ludunits2 -lm -ldl (cd test; make -f vVS.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vVS.o clang++ -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib (cd examples; make) mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_AGARD445_PyTest.py cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr2_PyTest.py cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Generic_Missile.py cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_PyTest.py cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_TipTreat_PyTest.py cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_AGARD445_PyTest.py cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Aeroelastic_PyTest.py cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Composite_PyTest.py cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Flutter_15degree.py cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_OptControl_PyTest.py cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_PyTest.py cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_ThreeBar_PyTest.py cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/astros_Trim_15degree.py cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/autoLink_Pytest.py cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_AutoSpan_PyTest.py cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_ControlSurf_PyTest.py cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_DesignSweep_PyTest.py cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_EigenValue_PyTest.py cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/avl_PyTest.py cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/awave_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_PyTest.py cp -p -f pyCAPS/cbaero_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cbaero_PyTest.py cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/delaundo_PyTest.py cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_PyTest.py cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/friction_PyTest.py cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_Morph_PyTest.py cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/fun3d_refine_PyTest.py cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_AGARD445_PyTest.py cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/masstran_PyTest.py cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mses_PyTest.py cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_AGARD445_PyTest.py cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_PyTest.py cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_AGARD445_PyTest.py cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Composite_PyTest.py cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Flutter_15degree.py cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PlateMisc_PyTest.py cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_PyTest.py cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_ThreeBar_PyTest.py cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/nastran_Trim_15degree.py cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py cp -p -f pyCAPS/plato_aflr_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_PyTest.py cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/plato_tetgen_table_PyTest.py cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_PyTest.py cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/pointwise_Symmetry_PyTest.py cp -p -f pyCAPS/su2_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_Morph_PyTest.py cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_X43a_PyTest.py cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR2_PyTest.py cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Delaundo_PyTest.py cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_Tetgen_PyTest.py cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_pointwise_PyTest.py cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Holes_PyTest.py cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_PyTest.py cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tetgen_Regions_PyTest.py cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/tsfoil_PyTest.py cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/pyCAPS/xfoil_PyTest.py cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/15degreeWing.csm cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransfer.csm cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/aeroelasticDataTransferSimple.csm cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/airfoilSection.csm cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.csm cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/avlWingTail.csm cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/avlWings.csm cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/awaveWingTailFuselage.csm cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2D.csm cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfd2DArbShape.csm cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfdMultiBody.csm cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfdSymmetry.csm cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfdX43a.csm cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cfd_airfoilSection.csm cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/compositeWing.csm cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_shell.csm cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/cyli_box_solid.csm cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaAGARD445.csm cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaBoxes.csm cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaCantileverPlate.csm cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaJoinedPlate.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaSimplePlate.csm cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaThreeBar.csm cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEM.csm cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/feaWingBEMAero.csm cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/frictionWingTailFuselage.csm cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/generic_missile.csm cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/interference.csm cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/linearAero.csm cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/nosecone1.csm cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/regions.csm cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/simpleWingBox.csm cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/spheres.csm cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/table.csm cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/tiptreat.csm cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/csmData/avlWing.udc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/boydBox.py cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/gp.py cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_blackbox.py cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/hoburg_gp.py cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/qp.py cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/sp.py cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing1.csm cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/csm/wing2.csm cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/csm/naca.csm cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Camber.py cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/MSES.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_CTestRegression.sh cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/execute_PyTestRegression.sh (make -C cCAPS -f aeroelastic_SU2.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awaveTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/frictionTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include interferenceTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/interferenceTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/mystranTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl +++ find /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training/ -name Makefile ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]] ++ continue ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//2023/data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//2023/data/session01 ++ make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/template_avl.o clang -g -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -lm -ldl ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/training//data/session01 ++ make make: Nothing to be done for `default'. ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/src ++ make -f serveESP.make clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/capsMode.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/capsMode.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flowchart.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flowchart.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timViewer.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/viewer.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/viewer.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.6 -I/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/include -I. -I. -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 -I/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPyscript.o touch /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pyscript.so rm /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pyscript.so clang++ -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/obj/timPyscript.o -L/usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin -lpython3.11 -ldl -framework CoreFoundation -L/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.6.0/./lib -Wl,-rpath /usr/local/opt/python@3.11/Frameworks/Python.framework/Versions/3.11/lib/python3.11/config-3.11-darwin ++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64 +++ find /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/OpenCSM/trunk/data/training/ -name Makefile + mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/test + cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/test + source /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/JenkinsESP/RunRegression.sh ++ [[ 0 == 1 ]] ++ [[ 0 == 2 ]] ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64 == '' ]] ++ [[ CAPS/LINEARAERO == '' ]] ++ [[ 7.6 == '' ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/examples/ ++ make test TYPE=LINEARAERO (make -C cCAPS -f aeroelastic_SU2.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. (make -C cCAPS -f avlTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/avlTest' is up to date. (make -C cCAPS -f awaveTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/awaveTest' is up to date. (make -C cCAPS -f frictionTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/frictionTest' is up to date. (make -C cCAPS -f fun3d.make) make[1]: Nothing to be done for `fun3d'. (make -C cCAPS -f hsm.make) make[1]: `hsm' is up to date. (make -C cCAPS -f interferenceTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/interferenceTest' is up to date. (make -C cCAPS -f msesTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/msesTest' is up to date. (make -C cCAPS -f mystran.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/mystranTest' is up to date. (make -C cCAPS -f pointwiseTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/cCAPS/pointwiseTest' is up to date. (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_CTestRegression.sh LINEARAERO) Running.... LINEARAERO c-Tests ================================================= + echo './avlTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt ./avlTest test; + ./avlTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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-01,2.965810831880e-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,-1.699095118252e-02,-7.589503463268e-04,7.958849673323e-03,1.019416065192e-02,8.688915578662e-03,6.053380335362e-03,5.120395027030e-03,9.296755297867e-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-01,8.167547094734e-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-01,8.948575908404e-01,9.327503738523e-01,9.379850374388e-01,9.144963748400e-01,8.662385668551e-01,7.987616435483e-01,7.207325646090e-01,6.617973538495e-01,6.363916792640e-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-03,1.893013552461e-02,2.388458719217e-02,2.809788812561e-02,3.450496926232e-02,4.310977683936e-02,5.296690620750e-02,6.273588035908e-02,7.092746653695e-02,7.623132904850e-02,7.793919402374e-02,1.330641046361e-01,7.642533954139e-02,1.575280561795e-02,1.020926164300e-02,5.734996040044e-03,2.453990236882e-03,7.034156944392e-05,-1.681061755697e-03,-2.904871637688e-03,-3.696799546922e-03,-4.291551637882e-03,-4.755989795808e-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":[-6.175122770636e-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,-7.889656776611e-02,-3.215621313961e-02],"cm_LE":[-9.907391078332e-02,-2.553625521061e-01,-3.443180862961e-01,-3.917771248736e-01,-4.170475207536e-01,-4.288879437378e-01,-4.309998082914e-01,-4.249313258859e-01,-4.112512348868e-01,-3.899661415022e-01,-3.610798550199e-01,-3.345295675168e-01,-3.190696575594e-01,-2.776668920570e-01,-2.496150543393e-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-01,5.217174153486e-01,5.035437183300e-01,4.956552889212e-01,4.999897967897e-01,5.161776906017e-01,5.451044281036e-01,5.898391652626e-01,6.538965497759e-01,7.352099770687e-01,8.201760893058e-01,8.930854083838e-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":[4.143502484418e-02,1.146121890397e-01,1.669674480704e-01,2.000258625574e-01,2.165069436647e-01,2.173612378313e-01,2.020982864238e-01,1.687203348324e-01,1.143884794128e-01,4.073751989356e-02],"ai":[2.065296924524e-01,1.849180223915e-01,1.591285664757e-01,1.456224964407e-01,1.435231644006e-01,1.506386553619e-01,1.666466052405e-01,1.914179167692e-01,2.193221173426e-01,2.365321328628e-01],"cl_norm":[6.579957348175e-02,1.763463053600e-01,2.425545992661e-01,2.698370559984e-01,2.694590983036e-01,2.501591871286e-01,2.170544160378e-01,1.714623014102e-01,1.118766125248e-01,3.907064104103e-02],"cl":[5.682537081788e-02,1.522949719002e-01,2.094733190132e-01,2.330348048801e-01,2.327083956798e-01,2.160407403860e-01,1.874510278160e-01,1.480770823176e-01,9.661810337317e-02,3.374191575671e-02],"cd":[4.670566079259e-03,1.374698956983e-02,1.845844898550e-02,2.032218684722e-02,2.072187092669e-02,2.023884851594e-02,1.896705322928e-02,1.657142171116e-02,1.222733795464e-02,5.106244760906e-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":[-3.303465544546e-02,-8.761746958841e-02,-1.194746602282e-01,-1.341488123562e-01,-1.380350789961e-01,-1.339349413679e-01,-1.218867053323e-01,-1.002593790934e-01,-6.716156843018e-02,-2.373448304332e-02],"cm_LE":[-4.232877133358e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490115e-01,-1.757829360722e-01,-1.683239687782e-01,-1.510824211715e-01,-1.228726806386e-01,-8.171902803714e-02,-2.878672165371e-02],"C.P.x/c":[8.313363814436e-01,8.253142634666e-01,8.203574125382e-01,8.256599853196e-01,8.431675932571e-01,8.699522420103e-01,9.002322593393e-01,9.270755982235e-01,9.451240614896e-01,9.534124326092e-01]} real 0m4.534s user 0m0.615s sys 0m0.369s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./avlTest passed (as expected) ============================================= ================================================= + echo './msesTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt ./msesTest test; + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt + ./msesTest 0 Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm Value of CL = 0.276892 real 0m4.850s user 0m2.932s sys 0m0.221s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./msesTest passed (as expected) ============================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt + echo './awaveTest test;' ./awaveTest test; + ./awaveTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 = 1.133332 0.216380 real 0m1.917s user 0m0.537s sys 0m0.241s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./awaveTest passed (as expected) ============================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/cCAPSlog.txt + echo './frictionTest test;' ./frictionTest test; + ./frictionTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 0m1.307s user 0m0.148s sys 0m0.085s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./frictionTest passed (as expected) ============================================= All tests pass! ================================================= ================================================= (cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest; ./execute_PyTestRegression.sh LINEARAERO) ================================================= Using python : /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python ================================================= Running.... LINEARAERO PyTests avl: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/avl ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 0.0006119078685748102 CYtot -6.295467348382128e-15 CZtot -0.3012861394885953 Cltot -4.784258926526785e-14 Cmtot -0.1945055953450382 Cntot -2.338191252215186e-15 Cl'tot -4.787610967125373e-14 Cn'tot -1.502866821492718e-15 CLtot 0.3012509314150635 CDtot 0.004646353488232475 CDvis 0.0 CLff 0.3009503023520388 CYff -7.723329422293541e-15 CDind 0.004646353488232475 CDff 0.004968969500907922 e 0.9669902146157789 StripForces Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -0.004234137764545] real 0m15.781s user 0m0.965s sys 0m0.822s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_AutoSpan_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 -0.04120015370850767 CYtot -2.245617010841538e-10 CZtot -1.125018809209926 Cltot -1.249787598356312e-09 Cmtot -1.954741267455616 Cntot 1.914701795830442e-10 Cl'tot -1.246255634256898e-09 Cn'tot 2.132528188740779e-10 CLtot 1.124128421568333 CDtot 0.06082816423346078 CDvis 0.0 CLff 1.123105443194628 CYff -2.724471052441854e-10 CDind 0.06082816423346078 CDff -0.2032091360675605 e -0.3293037505974324 real 0m20.137s user 0m19.173s sys 0m2.943s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_DesignSweep_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_DesignSweep_PyTest.py test; + python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 Cl[0] = 0.2009337808875886 Cd[0] = 0.002572533601556616 real 2m2.748s user 0m28.849s sys 0m36.345s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_ControlSurf_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 -0.01911479917643664 CYtot 0.03828770401119252 CZtot -0.6203123021542157 Cltot 0.0580302054292887 Cmtot -0.3649415791577237 Cntot -0.02051317548235195 Cl'tot 0.05766336287208888 Cn'tot -0.0215228179571592 CLtot 0.6198842263418534 CDtot 0.02993783031517985 CDvis 0.0 CLff 0.6192452092597066 CYff 0.0328707962584744 CDind 0.02993783031517985 CDff 0.02861019822661097 e 0.7130586920544685 real 0m2.001s user 0m0.954s sys 0m0.805s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_EigenValue_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO 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 0m1.472s user 0m0.745s sys 0m0.687s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_OpenMDAO_3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt avl_OpenMDAO_3_PyTest.py test; + python -u avl_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt 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 [2.19764579e-12] Cmtot2_Alpha [[4.24793143e-06]] Cmtot2_Beta [[6.71418674e-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 = 2.1976457892812188E-012 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-5.50424967] [2.89504288] real 0m56.053s user 0m4.313s sys 0m2.625s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected) ================================================= awave: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/awave ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt + echo 'awave_PyTest.py test;' awave_PyTest.py test; + python -u awave_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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 = [1.13333201, 0.216380075] real 0m1.240s user 0m0.780s sys 0m0.395s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected) ================================================= friction: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/friction ================================================= + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/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] real 0m1.182s user 0m0.573s sys 0m0.328s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= tsfoil2: /Users/jenkins/util/tsfoil/tsfoil2 ================================================= + echo 'tsfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Getting results PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Cl = 0.933417 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203436 Cp _Critcal = -1.303869 real 0m1.135s user 0m0.540s sys 0m0.252s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= mses: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/mses ================================================= + echo 'mses_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Cl = 0.37837932402995744 Cd = 0.0077758580442312715 Cm = 0.005262576090327783 real 0m5.078s user 0m4.088s sys 0m0.557s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_OpenMDAO_3_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt mses_OpenMDAO_3_PyTest.py test; + python -u mses_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt 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 [[0.17647556]] 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 [-0.07647556] CD [0.01022329] CD_camber [[-0.08760106]] At iterate 1 f= 1.02233D-02 |proj g|= 8.76011D-02 camber [-0.01793405] CD [0.00770371] CD_camber [[-0.01328824]] At iterate 2 f= 7.70371D-03 |proj g|= 1.32882D-02 camber [-0.00746595] CD [0.00760241] CD_camber [[-0.00542349]] At iterate 3 f= 7.60241D-03 |proj g|= 5.42349D-03 camber [-0.00024721] CD [0.00758207] CD_camber [[-0.00011833]] At iterate 4 f= 7.58207D-03 |proj g|= 1.18327D-04 camber [-8.62005111e-05] CD [0.00758208] CD_camber [[-3.2293282e-06]] camber [-0.00022068] CD [0.00758207] CD_camber [[-0.00010202]] At iterate 5 f= 7.58207D-03 |proj g|= 1.02022D-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 7 5 0 0 1.020D-04 7.582D-03 F = 7.5820696804286096E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.00022068] real 0m34.702s user 0m30.621s sys 0m2.267s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected) ================================================= xfoil: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/bin/xfoil ================================================= + echo 'xfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt Cl = [1.05475230553347, 1.36488869373699, 1.5660721427216, 2.03059709348412, 1.97271083121139, 1.87307153172667, 1.7605047576018] Cd = [0.0131991208677172, 0.0166540240605863, 0.0200551482562954, 0.0458671341943513, 0.07542560093961, 0.099446917447585, 0.127479430989108] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.496044115314418, 0.46137773204142, 0.442376568201556, 0.361251636297643, 0.276104140853528, 0.214381239319783, 0.132988264746104] real 0m7.479s user 0m6.247s sys 0m0.470s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= awave: /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/test/awave ================================================= + echo 'autoLink_Pytest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + python -u autoLink_Pytest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt 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 = [[0.01954019062669573, 0.017418911634864816, 0.016377545441609825, 0.015723407368881122, 0.015299766341236209, 0.015051258605772486, 0.014977771651911904], [0.02003019062669573, 0.017828911634864816, 0.016737545441609825, 0.016063407368881122, 0.01561976634123621, 0.015351258605772486, 0.015267771651911904], [0.02057019062669573, 0.018268911634864816, 0.017127545441609823, 0.01642340736888112, 0.01594976634123621, 0.015671258605772485, 0.015577771651911904], [0.02114019062669573, 0.018738911634864814, 0.017547545441609823, 0.016813407368881123, 0.01631976634123621, 0.016011258605772485, 0.015907771651911904], [0.02177019062669573, 0.019248911634864814, 0.018007545441609825, 0.017233407368881123, 0.01671976634123621, 0.016391258605772483, 0.016267771651911903], [0.02246019062669573, 0.019808911634864815, 0.018507545441609825, 0.01769340736888112, 0.017139766341236207, 0.016801258605772484, 0.016657771651911905], [0.02321019062669573, 0.020418911634864815, 0.019047545441609824, 0.018193407368881122, 0.01760976634123621, 0.017241258605772483, 0.017077771651911905], [0.02425019062669573, 0.021258911634864815, 0.019797545441609825, 0.018873407368881122, 0.01824976634123621, 0.017851258605772486, 0.017657771651911906], [0.02543019062669573, 0.022218911634864814, 0.020637545441609825, 0.019653407368881125, 0.018979766341236208, 0.018531258605772483, 0.018307771651911903], [0.02671019062669573, 0.023248911634864814, 0.021547545441609826, 0.020483407368881122, 0.019759766341236207, 0.019271258605772484, 0.019007771651911906], [0.02810019062669573, 0.024358911634864814, 0.02252754544160982, 0.02138340736888112, 0.02058976634123621, 0.020061258605772483, 0.019757771651911907], [0.02959019062669573, 0.025548911634864814, 0.023577545441609823, 0.022333407368881127, 0.02148976634123621, 0.020901258605772483, 0.020557771651911905]] real 1m46.728s user 1m19.234s sys 0m21.243s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* All tests pass! ================================================= ================================================= ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest ++ ./execute_PyTestRegression.sh LINEARAERO ================================================= Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/ESP/venv/bin/python ================================================= Running.... LINEARAERO PyTests ================================================= + rm -rf avl_PyTest + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 0.0006119078685748102 CYtot -6.295467348382128e-15 CZtot -0.3012861394885953 Cltot -4.784258926526785e-14 Cmtot -0.1945055953450382 Cntot -2.338191252215186e-15 Cl'tot -4.787610967125373e-14 Cn'tot -1.502866821492718e-15 CLtot 0.3012509314150635 CDtot 0.004646353488232475 CDvis 0.0 CLff 0.3009503023520388 CYff -7.723329422293541e-15 CDind 0.004646353488232475 CDff 0.004968969500907922 e 0.9669902146157789 StripForces Wing cl = [0.02994790451347, 0.08555545178933, 0.1329003532587, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.3101221284189, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805664, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996427, 0.2453427152623, 0.2100182422921, 0.17330251928, 0.1329003532723, 0.08555545180787, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653192, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946409, 0.000511459807839, 0.0021191472861, 0.004145189908974, 0.006609094404181, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.006609094404439, 0.00414518990926, 0.002119147286384, 0.0005114598080993, -0.0007386538944077, -0.001762021024096, -0.002739626801367, -0.003752887372445, -0.004494543653162, -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 0m2.359s user 0m0.894s sys 0m1.053s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Loading AIM ERROR:: (name_not_found) in Branch Brch_000083 at [[/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/csmData/avlWing.udc:114]] storage "Wing1Hinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000097 at [[/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/csmData/avlWing.udc:138]] storage "Wing1Hinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000209 at [[/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/csmData/avlWing.udc:114]] storage "Wing2Hinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000223 at [[/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/csmData/avlWing.udc:138]] storage "Wing2Hinge" 1 not found --> catching signal -251 (name_not_found) ERROR:: (name_not_found) in Branch Brch_000349 at [[/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/csmData/avlWing.udc:138]] storage "Wing3Hinge" 3 not found --> catching signal -251 (name_not_found) 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 -0.03128890285048182 CYtot -1.678460526101188e-10 CZtot -1.0146631556837 Cltot -9.601885758998949e-10 Cmtot -2.941985206618916 Cntot 1.607653278685522e-10 Cl'tot -9.572365926860225e-10 Cn'tot 1.774984438134748e-10 CLtot 1.013962550920935 CDtot 0.04899245118895509 CDvis 0.0 CLff 1.01275360566329 CYff -2.082410267409873e-10 CDind 0.04899245118895509 CDff -0.08941630295456776 e -0.6085408393538471 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.closeCAPS' is deprecated. Please use 'close'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! real 0m20.622s user 0m18.871s sys 0m3.247s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_DesignSweep_PyTest.py test; + python -u avl_DesignSweep_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 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 = 0.002572533601556616 Cl = 0.2009337808875886 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 = 0.002586364230247675 Cl = 0.2015191856817219 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 = 0.002609799718822078 Cl = 0.2025075296435699 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 = 0.002643444008430607 Cl = 0.2039185811661163 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 = 0.002688200921004275 Cl = 0.2057816377792995 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 = 0.002745342060022128 Cl = 0.2081373840562387 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 = 0.002816610334305089 Cl = 0.2110406736708028 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 = 0.002904376657741203 Cl = 0.2145646488018499 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 = 0.003011879793049438 Cl = 0.2188068842337489 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 = 0.003143602034593163 Cl = 0.2238987294818322 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 = 0.003305877285459588 Cl = 0.2300199286489811 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 = 0.003507917885480122 Cl = 0.237422386029936 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 = 0.003763643677267996 Cl = 0.2464707142747725 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 = 0.004095167898235787 Cl = 0.2577158067750623 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 = 0.004540047408144598 Cl = 0.2720394012166634 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 = 0.005168237926862041 Cl = 0.290970150746647 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 = 0.006128930715340515 Cl = 0.3174875485939014 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 = 0.00781835905128463 Cl = 0.3586078919922491 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 = 0.01186220444375424 Cl = 0.4382638635248127 Cl[0] = 0.2009337808875886 Cd[0] = 0.002572533601556616 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 1m36.008s user 0m30.842s sys 0m38.798s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf avl_ControlSurf_PyTest + echo 'avl_ControlSurf_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/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 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 -0.01911479917643664 CYtot 0.03828770401119252 CZtot -0.6203123021542157 Cltot 0.0580302054292887 Cmtot -0.3649415791577237 Cntot -0.02051317548235195 Cl'tot 0.05766336287208888 Cn'tot -0.0215228179571592 CLtot 0.6198842263418534 CDtot 0.02993783031517985 CDvis 0.0 CLff 0.6192452092597066 CYff 0.0328707962584744 CDind 0.02993783031517985 CDff 0.02861019822661097 e 0.7130586920544685 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 0m3.775s user 0m1.042s sys 0m1.046s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO 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 0m3.022s user 0m0.744s sys 0m0.845s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 = [1.13333201, 0.216380075] 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 0m2.088s user 0m0.784s sys 0m0.413s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf friction_PyTest + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 0m1.706s user 0m0.558s sys 0m0.379s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf tsfoil_PyTest + echo 'tsfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running tsFoil...... PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Getting results Cl = 0.933417 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203436 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 0m1.553s user 0m0.571s sys 0m0.298s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running xFoil...... Cl = [1.05475230553347, 1.36488869373699, 1.5660721427216, 2.03059709348412, 1.97271083121139, 1.87307153172667, 1.7605047576018] Cd = [0.0131991208677172, 0.0166540240605863, 0.0200551482562954, 0.0458671341943513, 0.07542560093961, 0.099446917447585, 0.127479430989108] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.496044115314418, 0.46137773204142, 0.442376568201556, 0.361251636297643, 0.276104140853528, 0.214381239319783, 0.132988264746104] 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 0m11.280s user 0m5.678s sys 0m0.487s + 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 /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + python -u autoLink_Pytest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64/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 = [[0.01954019062669573, 0.017418911634864816, 0.016377545441609825, 0.015723407368881122, 0.015299766341236209, 0.015051258605772486, 0.014977771651911904], [0.02003019062669573, 0.017828911634864816, 0.016737545441609825, 0.016063407368881122, 0.01561976634123621, 0.015351258605772486, 0.015267771651911904], [0.02057019062669573, 0.018268911634864816, 0.017127545441609823, 0.01642340736888112, 0.01594976634123621, 0.015671258605772485, 0.015577771651911904], [0.02114019062669573, 0.018738911634864814, 0.017547545441609823, 0.016813407368881123, 0.01631976634123621, 0.016011258605772485, 0.015907771651911904], [0.02177019062669573, 0.019248911634864814, 0.018007545441609825, 0.017233407368881123, 0.01671976634123621, 0.016391258605772483, 0.016267771651911903], [0.02246019062669573, 0.019808911634864815, 0.018507545441609825, 0.01769340736888112, 0.017139766341236207, 0.016801258605772484, 0.016657771651911905], [0.02321019062669573, 0.020418911634864815, 0.019047545441609824, 0.018193407368881122, 0.01760976634123621, 0.017241258605772483, 0.017077771651911905], [0.02425019062669573, 0.021258911634864815, 0.019797545441609825, 0.018873407368881122, 0.01824976634123621, 0.017851258605772486, 0.017657771651911906], [0.02543019062669573, 0.022218911634864814, 0.020637545441609825, 0.019653407368881125, 0.018979766341236208, 0.018531258605772483, 0.018307771651911903], [0.02671019062669573, 0.023248911634864814, 0.021547545441609826, 0.020483407368881122, 0.019759766341236207, 0.019271258605772484, 0.019007771651911906], [0.02810019062669573, 0.024358911634864814, 0.02252754544160982, 0.02138340736888112, 0.02058976634123621, 0.020061258605772483, 0.019757771651911907], [0.02959019062669573, 0.025548911634864814, 0.023577545441609823, 0.022333407368881127, 0.02148976634123621, 0.020901258605772483, 0.020557771651911905]] 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 2m40.883s user 1m27.961s sys 0m36.433s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* All tests pass! ================================================= ================================================= [Execution node] check if [macys_VM] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] 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: '/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/DARWIN64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.6,ESPTEST=CAPS/LINEARAERO,ESP_ARCH=DARWIN64,buildnode=macys_VM #619'. [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