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Started by upstream project "ESP_RegCaps" build number 632 originally caused by: Started by an SCM change Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on viggen in workspace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64 [WS-CLEANUP] Deleting project workspace... Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS doesn't exist Cleaning local Directory EGADS Checking out svn+ssh://acdl.mit.edu/home/svnroot/EGADS at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A trunk A trunk/docs A trunk/docs/EGADS_ref AU trunk/docs/EGADS_ref/egads.pdf A trunk/docs/EGADS_ref/egads.tex A trunk/docs/EGADS_ref/Makefile A trunk/docs/EGADS_ref/BEAMERoptions.tex A trunk/docs/EGADS_ref/beamercolorthemeacdl.sty AU trunk/docs/EGADS_ref/esp_logo.png A trunk/docs/ESPconcepts AU trunk/docs/ESPconcepts/Concepts.pdf A trunk/docs/ESPconcepts/Concepts.tex A trunk/docs/ESPconcepts/Makefile AU trunk/docs/ESPconcepts/bracket.png AU trunk/docs/ESPconcepts/efinal.png AU trunk/docs/ESPconcepts/efinalGrid.png AU trunk/docs/ESPconcepts/start.png AU trunk/docs/ESPconcepts/startGrid.png AU trunk/docs/ESPconcepts/temp.png AU trunk/docs/ESPconcepts/tempGrid.png AU trunk/docs/ESPconcepts/vGeom.png AU trunk/docs/ESPconcepts/vTess.png AU trunk/docs/ESPconcepts/caps_logo.png AU trunk/docs/ESPconcepts/esp_logo.png AU trunk/docs/ESPconcepts/oml.png AU trunk/docs/ESPconcepts/manifold.png AU trunk/docs/ESPconcepts/midplane.png A trunk/docs/ESPconcepts/beamercolorthemeacdl.sty AU trunk/docs/ESPconcepts/crossSections.png A trunk/docs/ESPconcepts/BEAMERoptions.tex AU trunk/docs/ESPconcepts/beam.png A trunk/docs/EGADS_dot AU trunk/docs/EGADS_dot/egads_dot.pdf A trunk/docs/EGADS_dot/egads_dot.tex AU trunk/docs/EGADS_dot/egads_dot_examples.pdf A trunk/docs/EGADS_dot/BEAMERoptions.tex A trunk/docs/EGADS_dot/Makefile A trunk/docs/EGADS_dot/beamercolorthemeacdl.sty A trunk/docs/EGADS_dot/egads_dot_examples.tex AU trunk/docs/EGADS_dot/esp_logo.png A trunk/docs/EGADS_dot/src A trunk/docs/EGADS_dot/src/NMakefile A trunk/docs/EGADS_dot/src/Makefile A trunk/docs/EGADS_dot/src/circle1_dot.c A trunk/docs/EGADS_dot/src/circle2_dot.c A trunk/docs/EGADS_dot/src/naca_dot.c A trunk/docs/EGADS_dot/src/ruled_naca_dot.c A trunk/docs/EGADS_dot/src/pingBodies.c A trunk/docs/EGADS_dot/csmListing.tex A trunk/docs/EGADS_dot/fig AU trunk/docs/EGADS_dot/fig/circle.pptx AU trunk/docs/EGADS_dot/fig/circle_input.png AU trunk/docs/EGADS_dot/fig/circle_ortho.png A trunk/docs/Tutorial A trunk/docs/Tutorial/Makefile AU trunk/docs/Tutorial/Tutorial.pdf A trunk/docs/Tutorial/Tutorial.tex A trunk/docs/Tutorial/egads2tri.c A trunk/docs/Tutorial/tire.c A trunk/docs/Tutorial/tire.py A trunk/docs/Tutorial/Tutorial.make A trunk/docs/Tutorial/tire.make A trunk/docs/Tutorial/BEAMERoptions.tex A trunk/docs/Tutorial/beamercolorthemeacdl.sty A trunk/docs/Tutorial/egads2tri.mak A trunk/docs/Tutorial/egads2tri.make AU trunk/docs/Tutorial/esp_logo.png AU trunk/docs/Tutorial/manifold.png A trunk/docs/Tutorial/tire.mak AU 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trunk/docs/UDP_UDF/figs/tire_edges.png AU trunk/docs/UDP_UDF/figs/tire_faces_1_5.png AU trunk/docs/UDP_UDF/figs/tire_faces_2_6.png AU trunk/docs/UDP_UDF/figs/tire_faces_3_4_7_8.png AU trunk/docs/UDP_UDF/figs/tire_filletted.png AU trunk/docs/UDP_UDF/figs/tire_final.png AU trunk/docs/UDP_UDF/figs/tire_nodes.png AU trunk/docs/UDP_UDF/figs/vGeom.png AU trunk/docs/UDP_UDF/figs/vTess.png AU trunk/docs/Viewer.pdf AU trunk/docs/Viewer.ppt A trunk/docs/EffectiveTopology.txt A trunk/docs/Motivation A trunk/docs/Motivation/BEAMERoptions.tex AU trunk/docs/Motivation/Motivation.pdf A trunk/docs/Motivation/Motivation.tex A trunk/docs/Motivation/beamercolorthemeesp.sty AU trunk/docs/Motivation/caps_logo.png AU trunk/docs/Motivation/cmpress A trunk/docs/Motivation/csmListing.tex AU trunk/docs/Motivation/esp_logo.png A trunk/docs/Motivation/figs AU trunk/docs/Motivation/figs/ChainRule.png AU trunk/docs/Motivation/figs/Coons.png AU trunk/docs/Motivation/figs/DARPA04.png AU trunk/docs/Motivation/figs/DARPA05.png AU trunk/docs/Motivation/figs/DesignProcess_Seriesv2.png AU trunk/docs/Motivation/figs/ESPscreen.png AU trunk/docs/Motivation/figs/FSI.png AU trunk/docs/Motivation/figs/Glider_fuse.png AU trunk/docs/Motivation/figs/Glider_twist.png AU trunk/docs/Motivation/figs/airfoils.png AU trunk/docs/Motivation/figs/bolt.png AU trunk/docs/Motivation/figs/coonsCADfig.png AU trunk/docs/Motivation/figs/fighter-BEM.png AU trunk/docs/Motivation/figs/fighter-MSA.png AU trunk/docs/Motivation/figs/fighter-OML.png AU trunk/docs/Motivation/figs/fighter-SSM.png AU trunk/docs/Motivation/figs/flaps.png AU trunk/docs/Motivation/figs/parametricViews.png AU trunk/docs/Motivation/figs/views.png A trunk/docs/FullAttribution.txt A trunk/include A trunk/include/egads.h A trunk/include/LINUX64 A trunk/include/LINUX_AARCH64 A trunk/include/WIN64.2017 A trunk/include/WIN64.2019 A trunk/include/WIN64.2022 A trunk/include/DARWIN64 A trunk/include/DARWIN64.gcc A trunk/include/DARWIN_ARM64 A trunk/include/DARWIN64.clang A trunk/include/LINUX64.gprof A trunk/include/egadsTypes.h A trunk/include/egads.inc A trunk/include/egadsErrors.h A trunk/include/egads_dot.h A trunk/include/egadsf90.inc A trunk/include/prm.h A trunk/include/wsserver.h A trunk/include/wsss.h AU trunk/include/CYGWIN64 A trunk/include/STANALYZER.make A trunk/include/emp.h A trunk/include/wsserver.inc A trunk/include/gv.h A trunk/include/gv.inc A trunk/include/Graphics.h A trunk/src A trunk/src/egadsCopy.cpp A trunk/src/fgadsTopo.c A trunk/src/egadsIO.cpp A trunk/src/egadsSBO.c A trunk/src/egadsGeom.cpp A trunk/src/egads.def A trunk/src/fgadsGeom.c A trunk/src/egadsSpline.cpp A trunk/src/egadsTopo.cpp A trunk/src/egadsBase.c A trunk/src/Makefile A trunk/src/egadsTessInp.c A trunk/src/egadsOCC.h A trunk/src/egadsClasses.h A trunk/src/egadsHLevel.cpp AU trunk/src/egads.rc A trunk/src/egadsAttrs.c A trunk/src/egadsEffect.c A trunk/src/egadsExport.c A trunk/src/egadsFit.c A trunk/src/egadsInternals.h A trunk/src/egadsMemory.c A trunk/src/egadsQuads.c A trunk/src/egadsSkinning.cpp A trunk/src/egadsSolids.c A trunk/src/egadsSplineFit.cpp A trunk/src/egadsSplineVels.h A trunk/src/egadsStack.h A trunk/src/egadsTess.c A trunk/src/egadsTessSens.cpp A trunk/src/egadsTris.c A trunk/src/egadsTris.h A trunk/src/fgadsAttrs.c A trunk/src/fgadsBase.c A trunk/src/fgadsHLevel.c A trunk/src/fgadsMemory.c A trunk/src/fgadsTess.c A trunk/src/fgv.c A trunk/src/prmCfit.c A trunk/src/prmGrid.c A trunk/src/prmUV.c A trunk/src/Surreal A trunk/src/Surreal/SurrealD_Lazy.h A trunk/src/Surreal/SurrealD_Trad.h A trunk/src/Surreal/SurrealS_Lazy.h A trunk/src/Surreal/SurrealS_Trad.h A trunk/src/Surreal/SurrealS.h A trunk/src/Surreal/SurrealD.h A trunk/src/Surreal/always_inline.h A trunk/src/OCC AU trunk/src/OCC/BRepLib_FuseEdges.cpp AU trunk/src/OCC/BRepLib_FuseEdges.h AU trunk/src/OCC/BRepPrimAPI_MakePrism.cpp AU trunk/src/OCC/BRepPrimAPI_MakePrism.hxx AU trunk/src/OCC/BRepPrimAPI_MakeRevol.cpp AU trunk/src/OCC/BRepPrimAPI_MakeRevol.hxx AU trunk/src/OCC/BRepSweep_Prism.cpp AU trunk/src/OCC/BRepSweep_Prism.hxx AU trunk/src/OCC/BRepSweep_Revol.cpp AU trunk/src/OCC/BRepSweep_Revol.hxx AU trunk/src/OCC/BRepSweep_Rotation.cpp AU trunk/src/OCC/BRepSweep_Rotation.hxx AU trunk/src/OCC/BRepSweep_Translation.cpp AU trunk/src/OCC/BRepSweep_Translation.hxx A trunk/src/NMakefile A trunk/src/egadsRobust.c AU trunk/src/elint A trunk/src/egadsSplineFit.h AU trunk/src/flint AU trunk/src/make.bat A trunk/config A trunk/config/linREADME.txt A trunk/config/macREADME.txt AU trunk/config/setup.cmd AU trunk/config/setup.command AU trunk/config/setup.sh A trunk/config/winREADME.txt A trunk/config/README.txt A trunk/config/MACdownloads.txt A trunk/config/WINdownloads.txt AU trunk/config/makeEnv AU trunk/config/winEnv A trunk/util A trunk/util/uvmap A trunk/util/uvmap/uvmap_gen_uv.c A trunk/util/uvmap/uvmap_bnd_adj.c A trunk/util/uvmap/uvmap_bnd_adj.h A trunk/util/uvmap/main A trunk/util/uvmap/main/uvmap.c A trunk/util/uvmap/Release_Notes_uvmap.txt A trunk/util/uvmap/UVMAP_LIB.h A trunk/util/uvmap/uvmap_gen.c A trunk/util/uvmap/uvmap_version.c A trunk/util/uvmap/Makefile.common AU trunk/util/uvmap/uvmap.compile_lib A trunk/util/uvmap/EG_uvmapTest.c A trunk/util/uvmap/EG_uvmapTest.h A trunk/util/uvmap/EG_uvmap_Read.c A trunk/util/uvmap/EG_uvmap_Read.h A trunk/util/uvmap/EG_uvmap_Write.c A trunk/util/uvmap/EG_uvmap_Write.h A trunk/util/uvmap/UVMAP_LIB_INC.h A trunk/util/uvmap/uvmap_read.c A trunk/util/uvmap/uvmap_test.c A trunk/util/uvmap/uvmap_test.h A trunk/util/uvmap/EG_uvmapFindUV.c A trunk/util/uvmap/EG_uvmapFindUV.h A trunk/util/uvmap/EG_uvmapGen.c A trunk/util/uvmap/EG_uvmapGen.h A trunk/util/uvmap/EG_uvmapStructFree.c A trunk/util/uvmap/EG_uvmapStructFree.h AU trunk/util/uvmap/OpenLicense.pdf A trunk/util/uvmap/OpenLicense.txt A trunk/util/uvmap/uvmap_chk_edge_ratio.c A trunk/util/uvmap/uvmap_chk_edge_ratio.h A trunk/util/uvmap/uvmap_message.c A trunk/util/uvmap/uvmap_solve.c A trunk/util/uvmap/uvmap_write.c A trunk/util/uvmap/uvmap_ibeibe.c A trunk/util/uvmap/uvmap_ibfibf.c A trunk/util/uvmap/uvmap_idibe.c A trunk/util/uvmap/Makefile.Cygwin A trunk/util/uvmap/Makefile.Linux A trunk/util/uvmap/Makefile.MacOSX A trunk/util/uvmap/uvmap_cpu_message.c A trunk/util/uvmap/uvmap_find_uv.c A trunk/util/uvmap/uvmap_find_uv.h AU trunk/util/uvmap/uvmap.compile AU trunk/util/uvmap/uvmap.lib_list A trunk/util/uvmap/uvmap_add.c A trunk/util/uvmap/uvmap_add.h A trunk/util/uvmap/uvmap_chk_area_uv.c A trunk/util/uvmap/uvmap_chk_area_uv.h A trunk/util/uvmap/uvmap_cpu_message.h A trunk/util/uvmap/uvmap_from_egads.c A trunk/util/uvmap/uvmap_from_egads.h A trunk/util/uvmap/uvmap_gen.h A trunk/util/uvmap/uvmap_gen_uv.h A trunk/util/uvmap/uvmap_ibeibe.h A trunk/util/uvmap/uvmap_ibfibf.h A trunk/util/uvmap/uvmap_ibfin.c A trunk/util/uvmap/uvmap_ibfin.h A trunk/util/uvmap/uvmap_iccibe.c A trunk/util/uvmap/uvmap_iccibe.h A trunk/util/uvmap/uvmap_iccin.c A trunk/util/uvmap/uvmap_iccin.h A trunk/util/uvmap/uvmap_idibe.h A trunk/util/uvmap/uvmap_inibe.c A trunk/util/uvmap/uvmap_inibe.h A trunk/util/uvmap/uvmap_inl_uv_bnd.c A trunk/util/uvmap/uvmap_inl_uv_bnd.h A trunk/util/uvmap/uvmap_malloc.c A trunk/util/uvmap/uvmap_malloc.h A trunk/util/uvmap/uvmap_mben_disc.c A trunk/util/uvmap/uvmap_mben_disc.h A trunk/util/uvmap/uvmap_message.h A trunk/util/uvmap/uvmap_norm_uv.c A trunk/util/uvmap/uvmap_norm_uv.h A trunk/util/uvmap/uvmap_read.h A trunk/util/uvmap/uvmap_solve.h A trunk/util/uvmap/uvmap_struct.h A trunk/util/uvmap/uvmap_struct_tasks.c A trunk/util/uvmap/uvmap_struct_tasks.h A trunk/util/uvmap/uvmap_to_egads.c A trunk/util/uvmap/uvmap_to_egads.h A trunk/util/uvmap/uvmap_version.h A trunk/util/uvmap/uvmap_write.h A trunk/util/egadsHOtess.c A trunk/util/egadsPatch.c A trunk/util/egadsPatch.h A trunk/util/egadsUVmap.c A trunk/util/evaluate.c A trunk/util/evaluateNR.c A trunk/util/extractTess.c A trunk/util/limitTessBody.c A trunk/util/retessFaces.c A trunk/util/vHOtess.c A trunk/util/SurrealD4_btest.cpp A trunk/util/regQuads.c A trunk/util/emp.c A trunk/util/SurrealD1_btest.cpp A trunk/util/SurrealS1_btest.cpp A trunk/util/SurrealS4_btest.cpp A trunk/util/ThreadTest.c A trunk/util/triServer.c A trunk/util/triServer.mak A trunk/util/triServer.make A trunk/util/vHOtess.mak A trunk/util/egadsPatch.mak A trunk/util/egadsPatch.make AU trunk/util/plint A trunk/util/NMakefile A trunk/util/rational.c A trunk/util/Makefile A trunk/util/README.txt A trunk/util/regQuads.h A trunk/util/extractTess.mak A trunk/util/extractTess.make A trunk/util/limits.mak AU trunk/util/HOlint A trunk/util/vHOtess.make A trunk/util/gp_Vec2d68.lxx A trunk/util/gp_Vec2d.lxx A trunk/util/limits.make AU trunk/util/ulint A trunk/test A trunk/test/addKnots.c A trunk/test/egadsSpline_dot.c A trunk/test/egadsGeom_dot.c A trunk/test/egadsGeom_dot.mak A trunk/test/egadsGeom_dot.make A trunk/test/egadsHLevel_dot.c A trunk/test/egadsHLevel_dot.mak A trunk/test/egadsHLevel_dot.make A trunk/test/egadsSpline_dot.mak A trunk/test/egadsSpline_dot.make A trunk/test/egadsTools_dot.c A trunk/test/egadsTools_dot.h A trunk/test/egadsTopo_dot.c A trunk/test/egadsTopo_dot.mak A trunk/test/egadsTopo_dot.make A trunk/test/globalTess.c A trunk/test/BSplineIGES.c A trunk/test/CSys.c A trunk/test/GBO.c A trunk/test/SBO.c A trunk/test/agglom.c A trunk/test/approx.f A trunk/test/blend.c A trunk/test/chamfer.c A trunk/test/closure.f A trunk/test/edge2WB.c A trunk/test/edges.c A trunk/test/effective.c A trunk/test/egads2cart.c A trunk/test/egads2ply.cpp A trunk/test/extrot.c A trunk/test/fillet.c A trunk/test/fit.c A trunk/test/fullAttr.c A trunk/test/fuseSheets.c A trunk/test/hollow.c A trunk/test/hollowFace.c A trunk/test/intersect.c A trunk/test/makeCone.c A trunk/test/makeFace3D.c A trunk/test/makeLoop.c A trunk/test/mofb.c A trunk/test/mssb.c A trunk/test/multiContext.c A trunk/test/offset.c A trunk/test/parsec.c A trunk/test/parsef.f A trunk/test/rebuild.c A trunk/test/refObj.c A trunk/test/replace.c A trunk/test/revolve.c A trunk/test/ruled.c A trunk/test/saveTess.c A trunk/test/scribe.c A trunk/test/sew.c A trunk/test/simplePer.c A trunk/test/smallEdges.c A trunk/test/step.f A trunk/test/sweep.c A trunk/test/testc.c A trunk/test/testf.f A trunk/test/tolerance.c A trunk/test/union.f A trunk/test/vAttr.c A trunk/test/vCurvature.c A trunk/test/vEffect.c A trunk/test/vEto.c A trunk/test/vFrame.c A trunk/test/vGeom.c A trunk/test/vQuad.c A trunk/test/vTess.c A trunk/test/vTessInp.c A trunk/test/xform.c A trunk/test/mapTess.c A trunk/test/refObj.make A trunk/test/simplePer.make AU trunk/test/runUnitTest.sh A trunk/test/vAttr.make A trunk/test/vCurvature.mak A trunk/test/vCurvature.make A trunk/test/vEffect.mak A trunk/test/vEffect.make A trunk/test/vEto.make A trunk/test/vFrame.make A trunk/test/vGeom.mak A trunk/test/vGeom.make A trunk/test/vQuad.make A trunk/test/vTess.mak A trunk/test/vTess.make A trunk/test/vTessInp.make A trunk/test/exportLite.mak A trunk/test/exportLite.make A trunk/test/saveTess.make A trunk/test/makeTests.bat A trunk/test/effective.make A trunk/test/smallEdges.make A trunk/test/fullAttr.mak A trunk/test/fullAttr.make A trunk/test/fitTri.c AU trunk/test/tinyply.cpp A trunk/test/egads2ply.make A trunk/test/approx.make A trunk/test/closure.make A trunk/test/step.make A trunk/test/test.make A trunk/test/union.make A trunk/test/edge2WB.make A trunk/test/GBO.make A trunk/test/multiContext.mak A trunk/test/multiContext.make A trunk/test/addKnots.make A trunk/test/sew.make AU trunk/test/tinyply.h A trunk/test/test.mak A trunk/test/SBO.make A trunk/test/fuseSheets.make A trunk/test/scribe.make A trunk/test/BSplineIGES.make A trunk/test/hollowFace.make A trunk/test/mssb.make A trunk/test/CSys.make A trunk/test/globalTess.make A trunk/test/blend.mak A trunk/test/chamfer.make A trunk/test/agglom.make A trunk/test/egads2cart.mak A trunk/test/ruled.make A trunk/test/revolve.make A trunk/test/makeFace3D.make A trunk/test/sweep.make A trunk/test/blend.make A trunk/test/hollow.make A trunk/test/makeLoop.make A trunk/test/mapTess.make A trunk/test/rebuild.make A trunk/test/fitTri.make A trunk/test/replace.make A trunk/test/tolerance.make A trunk/test/mofb.make A trunk/test/edges.make A trunk/test/xform.make A trunk/test/fillet.make A trunk/test/egads2cart.make A trunk/test/makeCone.make A trunk/test/fit.make A trunk/test/extrot.make A trunk/test/offset.make A trunk/test/intersect.make A trunk/test/Piston.BRep A trunk/test/misc1.step A trunk/test/iges2.igs A trunk/jlEGADS A trunk/jlEGADS/egads A trunk/jlEGADS/egads/Makefile A trunk/jlEGADS/egads/src A trunk/jlEGADS/egads/src/egads.jl A trunk/jlEGADS/egads/test A trunk/jlEGADS/egads/test/runtests.jl A trunk/jlEGADS/egads/test/Project.toml A trunk/jlEGADS/egads/Project.toml A trunk/jlEGADS/egads/README.txt A trunk/jlEGADS/egads/USAGE.txt A trunk/jlEGADS/egadslite A trunk/jlEGADS/egadslite/Makefile A trunk/jlEGADS/egadslite/Project.toml A trunk/jlEGADS/egadslite/src A trunk/jlEGADS/egadslite/src/egadslite.jl A trunk/jlEGADS/egadslite/test A trunk/jlEGADS/egadslite/test/Project.toml A trunk/jlEGADS/egadslite/test/runtests.jl A trunk/jlEGADS/egadscommon A trunk/jlEGADS/egadscommon/Makefile A trunk/jlEGADS/egadscommon/build.jl A trunk/jlEGADS/egadscommon/egadscommon.jl A trunk/jlEGADS/Makefile A trunk/pyEGADS A trunk/pyEGADS/pyEGADS A trunk/pyEGADS/pyEGADS/egads.py A trunk/pyEGADS/pyEGADS/egads_common.py A trunk/pyEGADS/pyEGADS/egadslite.py A trunk/pyEGADS/pyEGADS/__init__.py A trunk/pyEGADS/test A trunk/pyEGADS/test/test_egads.py A trunk/pyEGADS/test/test_egadslite.py A trunk/pyEGADS/test/Makefile A trunk/pyEGADS/test/NMakefile A trunk/lite A trunk/lite/egadsXsect.c AU trunk/lite/egadslite.rc A trunk/lite/inFace.c A trunk/lite/liteAttrs.c A trunk/lite/liteBase.c A trunk/lite/liteClasses.h A trunk/lite/liteGeom.c A 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2034 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS doesn't exist Cleaning local Directory CAPS Checking out svn+ssh://acdl.mit.edu/home/svnroot/CAPS at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A aim A aim/utils A aim/utils/cfdTypes.h A aim/utils/cfdUtils.c AU aim/utils/feaUtils.c AU aim/utils/feaTypes.h AU aim/utils/feaUtils.h AU aim/utils/jsonUtils.c AU aim/utils/nastranUtils.c A aim/utils/meshUtils.h AU aim/utils/nastranUtils.h A aim/utils/Makefile A aim/utils/meshUtils.c AU aim/utils/cardUtils.c AU aim/utils/cardUtils.h A aim/utils/miscUtils.c A aim/utils/miscUtils.h AU aim/utils/nastranCards.c AU aim/utils/nastranCards.h AU aim/utils/vlmTypes.h AU aim/utils/vlmUtils.c AU aim/utils/vlmUtils.h AU aim/utils/jsonUtils.h AU 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data/csmIgnore_7.4.txt A data/csmIgnore_7.6.txt A data/csmIgnore_7.7.txt A data/csmIgnore_7.8.txt A data/csmOCCFailure_7.3.txt A data/csmOCCFailure_7.4.txt A data/csmOCCFailure_7.6.txt A data/csmOCCFailure_7.7.txt A data/csmOCCFailure_7.8.txt A data/egadsTessError.txt A data/gallery A data/gallery/csmErrorHandling.txt A data/gallery/csmOCCFailure_7.3.txt A data/gallery/csmOCCFailure_7.4.txt A data/gallery/csmOCCFailure_7.6.txt A data/gallery/csmOCCFailure_7.7.txt A data/gallery/csmOCCFailure_7.8.txt A data/gallery/egadsTessError.txt A data/legacy A data/legacy/csmErrorHandling.txt A data/legacy/csmOCCFailure_7.3.txt A data/legacy/csmOCCFailure_7.4.txt A data/legacy/csmOCCFailure_7.6.txt A data/legacy/csmOCCFailure_7.7.txt A data/legacy/csmOCCFailure_7.8.txt A data/legacy/egadsTessError.txt A data/plugs A data/plugs/plugsFailure.txt A data/plugs/plugsIgnore.txt A data/plugs/plugsIgnoreValgrind.txt A data/sensFailure.txt A data/studentGallery A data/studentGallery/csmErrorHandling.txt A data/studentGallery/csmOCCFailure_7.3.txt A data/studentGallery/csmOCCFailure_7.4.txt A data/studentGallery/csmOCCFailure_7.6.txt A data/studentGallery/csmOCCFailure_7.7.txt A data/studentGallery/csmOCCFailure_7.8.txt A data/studentGallery/egadsTessError.txt A data/training A data/training/csmErrorHandling.txt A data/training/csmOCCFailure_7.3.txt A data/training/csmOCCFailure_7.4.txt A data/training/csmOCCFailure_7.6.txt A data/training/csmOCCFailure_7.7.txt A data/training/csmOCCFailure_7.8.txt A data/training/egadsTessError.txt A data/vsp3 A data/vsp3/csmErrorHandling.txt A data/vsp3/csmOCCFailure_7.6.txt A data/vsp3/csmOCCFailure_7.7.txt A data/vsp3/csmOCCFailure_7.8.txt A data/vsp3/egadsTessError.txt AU expectCSM.sh AU expectPLUGS.sh AU expectSENS.sh AU expectSLUGS.sh A splitCSMFiles.sh A suppression_address.txt A suppression_undefined.txt A test_pyOCSM.sh A tex A tex/BEAMERoptions.tex AU tex/JenkinsESP.pdf A tex/JenkinsESP.tex A tex/beamercolorthemeacdl.sty A valgrind A valgrind/valgrind-AFLR.supp A valgrind/valgrind-IRIT.supp A valgrind/valgrind-MKL.supp A valgrind/valgrind-OCC7.3.supp A valgrind/valgrind-OCC7.4.supp A valgrind/valgrind-OCC7.6.supp A valgrind/valgrind-OCC7.7.supp A valgrind/valgrind-OCC7.8.supp A valgrind/valgrind-Tblade3.supp A valgrind/valgrind-Ubuntu.supp A valgrind/valgrind-exodus.supp A valgrind/valgrind-python.supp A valgrind_command.sh At revision 851 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/src doesn't exist Cleaning local Directory OpenCSM/trunk/src Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A OpenCSM.c A OpenCSM.h A timPyscript.c A Makefile.DARWIN64 A udpCsm.c A Makefile A udpVsp3.c A checkVtk.c A vtk2stl.c A udfOffset.c A udfGanged.c A udfCreateBEM.c A udfDroop.c AU ocsm.rc A serveESP.c A udpSample.c A udpUtilities.c A OpenCSMtcl.c A OpenCSMtcl.h A adjointCSM.c A buildCSM.c A common.h A compareVerify.c A egg.h A eggPDT2.c A esp.h A fun3dCSM.c A gmgwCSM.c A gridCSM.c A liteCSM.c A massProps.c A matchCSM.c A naca456.f90 A parka.c A sensCSM.c A serveCSM.c A simpleCSM.cpp A tessCSM.c A tim.c A tim.h A timCapsMode.c A timEreped.c A timFlowchart.c A timGloves.c A timMitten.c A timPlotter.c A timPlugs.c A timSlugs.c A timViewer.c A timVspSetup.c A udfCatmull.c A udfCompare.c A udfCreatePoly.c A udfDeform.c A udfDroop2.c A udfDroop3.c A udfDumpPmtrs.c A udfEditAttr.c A udfFlend.c A udfGuide.c A udfLinalg.c A udfMatchBodys.c A udfMechanism.c A udfNaca6mc.c A udfNacelle.c A udfNuscale.c A udfPrintBbox.c A udfPrintBrep.c A udfPrintEgo.c A udfShadow.c A udfSlices.c A udfStiffener.c A udfTester1.c A udfTile.c A udfTile2.c A udp.c A udp.h A udpBezier.c A udpBiconvex.c A udpBox.c A udpBspline.c A udpEllipse.c A udpEqn2body.c A udpFitcurve.c A udpFreeform.c A udpGlovesBox.c A udpGlovesCyl.c A udpGlovesFuse.c A udpGlovesSphr.c A udpGlovesVtail.c A udpGlovesWing.c A udpHex.c A udpImport.c A udpKulfan.c A udpLevelset.c A udpNaca.c A udpNaca456.c A udpNurbbody.c A udpParabaloid.c A udpParsec.c_original A udpParsec.cpp A udpPod.c A udpPoly.c A udpProp.c A udpRadwaf.c A udpSew.c A udpStag.c A udpSupell.c A udpTblade.c A udpTester2.c A udpUtilities.h A udpVspComp.c A udpVspFuse.c A udpWaffle.c A udpWarp.c A vsp2csm.c A udfTile.make A udp.def A Makefile.DARWIN64.gcc A udp.help A udpHubWedge.c A Makefile.LINUX64 A NMakefile A serveESP.mak A ocsm.def A serveESP.make A timPyscript.def A timGloves.h A tim.def A Tblade3 A Tblade3/3dbgb.f90 A Tblade3/bladegen.f90 A Tblade3/bladestack.f90 A Tblade3/bsplinecam.f90 A Tblade3/derivatives.f90 A Tblade3/file_operations.f90 A Tblade3/funcNsubs.f90 A Tblade3/globvar.f90 A Tblade3/readinput.f90 A Tblade3/Makefile A Tblade3/Makefile.DARWIN64 A Tblade3/Makefile.LINUX64 A Tblade3/MakefileESP A Tblade3/cubicspline.f90 A Tblade3/errors.f90 A Tblade3/spanwise_variation.f90 A Tblade3/spline.f90 A Tblade3/bspline3.f90 A Tblade3/NMakefile A Tblade3/airfoiltypes.f90 A Tblade3/splinethick.f90 A Tblade3/techop.f90 A Tblade3/3dbgb_driver.f90 A Tblade3/T-Blade3_ReadMe.txt A Tblade3/T-Blade3_ReadMe_ESP.txt A Tblade3/license.txt A Tblade3/GitHub.address A udfTile.mak A udfTile2.mak A udfTile2.make A tcl AU tcl/buildCSM2.tcl A tcl/sketcher.tcl A udfCompare.mak A udfCompare.make A OpenCSM.help A egg.def A RunAllCsmFiles.bat U . At revision 2476 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/udc doesn't exist Cleaning local Directory OpenCSM/trunk/udc Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A flapz.udc A splitEdges.udc A combine.udc A replicate.udc A wing.udc A applyTparams.udc A contains.udc A overlaps.udc A glovesFuse.udc A glovesVtail.udc A glovesWing.udc A swap.udc A viewAvl.udc A gen_rot.udc A viewSansLIP.udc A viewSkinStructure.udc A capsHeader.udc A capsViews.udc A viewAstros.udc A viewConcept.udc A viewMasstran.udc A viewSu2Inviscid.udc A viewSu2Viscous.udc A duct.udc A strut.udc A wake.udc A fuselage.udc A popupz.udc A biconvex.udc A boxudc.udc A spoilerz.udc A diamond.udc A expressions.udc At revision 2476 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/data doesn't exist Cleaning local Directory OpenCSM/trunk/data Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A basic A basic/boolTest1a.csm A basic/boolTest1b.csm A basic/boolTest1c.csm A basic/boolTest1d.csm A basic/boolTest1e.csm A basic/boolTest1f.csm A basic/boolTest2a.csm A basic/boolTest2b.csm A basic/boolTest2c.csm A basic/boolTest2d.csm A basic/boolTest2e.csm A basic/boolTest2f.csm A basic/boolTest2g.csm A basic/boolTest2h.csm A basic/boolTest2i.csm A basic/boolTest2j.csm A basic/boolTest3a.csm A basic/boolTest3b.csm A basic/boolTest4a.csm A basic/boolTest4b.csm A basic/scribe11x.csm A basic/scribe11y.csm A basic/scribe11z.csm A basic/subtract6d.csm A basic/subtract6e.csm A basic/verify_7.6.0 A basic/verify_7.6.0/boolTest1a.vfy A basic/verify_7.6.0/boolTest1b.vfy A basic/verify_7.6.0/boolTest1c.vfy A basic/verify_7.6.0/boolTest1d.vfy A basic/verify_7.6.0/boolTest1e.vfy A basic/verify_7.6.0/boolTest1f.vfy A basic/verify_7.6.0/boolTest2a.vfy A basic/verify_7.6.0/boolTest2b.vfy A basic/verify_7.6.0/boolTest2c.vfy A basic/verify_7.6.0/boolTest2d.vfy A basic/verify_7.6.0/boolTest2e.vfy A basic/verify_7.6.0/boolTest2f.vfy A basic/verify_7.6.0/boolTest2g.vfy A basic/verify_7.6.0/boolTest2h.vfy A basic/verify_7.6.0/boolTest2i.vfy A basic/verify_7.6.0/boolTest2j.vfy A basic/verify_7.6.0/boolTest3a.vfy A basic/verify_7.6.0/boolTest3b.vfy A basic/verify_7.6.0/boolTest4a.vfy A basic/verify_7.6.0/boolTest4b.vfy A basic/verify_7.6.0/plateHoles1.vfy A basic/verify_7.6.0/plateHoles2.vfy A basic/verify_7.6.0/scribe11x.vfy A basic/verify_7.6.0/scribe11y.vfy A basic/verify_7.6.0/scribe11z.vfy A basic/verify_7.6.0/scribe12a.vfy A basic/verify_7.6.0/scribe12b.vfy A basic/verify_7.6.0/subtract6b.vfy A basic/verify_7.6.0/subtract6c.vfy A basic/verify_7.6.0/blend32a.vfy A basic/verify_7.6.0/blend32b.vfy A basic/verify_7.6.0/blend32c.vfy A basic/verify_7.6.0/nuscale5a.vfy A basic/verify_7.6.0/nuscale5b.vfy A basic/verify_7.6.0/nuscale6a.vfy A basic/verify_7.6.0/nuscale6b.vfy A basic/verify_7.6.0/nuscale7a.vfy A basic/verify_7.6.0/nuscale7b.vfy A basic/verify_7.6.0/nuscale8a.vfy A basic/verify_7.6.0/nuscale8b.vfy A basic/verify_7.6.0/blend31a.vfy A basic/verify_7.6.0/blend31b.vfy A basic/verify_7.6.0/blend31c.vfy A basic/verify_7.6.0/blend31d.vfy A basic/verify_7.6.0/winglet1.vfy A basic/verify_7.6.0/winglet2.vfy A basic/verify_7.6.0/clearance1.vfy A basic/verify_7.6.0/clearance2.vfy A basic/verify_7.6.0/clearance3.vfy A basic/verify_7.6.0/periodicFit.vfy A basic/verify_7.6.0/persist3a.vfy A basic/verify_7.6.0/persist3b.vfy A 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basic/verify_7.6.0/rule30f.vfy A basic/verify_7.6.0/group5.vfy A basic/verify_7.6.0/capNacelle1.vfy A basic/verify_7.6.0/capNacelle2.vfy A basic/verify_7.6.0/testAdjoint6.vfy A basic/verify_7.6.0/testAdjoint7.vfy A basic/verify_7.6.0/testAdjoint5.vfy A basic/verify_7.6.0/testAdjoint4.vfy A basic/verify_7.6.0/testAdjoint4.vfy_hand A basic/verify_7.6.0/testAdjoint5.vfy_hand A basic/verify_7.6.0/areaRule1.vfy A basic/verify_7.6.0/areaRule2.vfy A basic/verify_7.6.0/design0c.tsen A basic/verify_7.6.0/design0r.tsen A basic/verify_7.6.0/design8b.tsen A basic/verify_7.6.0/design9.tsen A basic/verify_7.6.0/designE2.tsen A basic/verify_7.6.0/designE3.tsen A basic/verify_7.6.0/designE4.tsen A basic/verify_7.6.0/designK0.tsen A basic/verify_7.6.0/designK1.tsen A basic/verify_7.6.0/designK2.tsen A basic/verify_7.6.0/designL00.tsen A basic/verify_7.6.0/designL01.tsen A basic/verify_7.6.0/designL10.tsen A basic/verify_7.6.0/designL11.tsen A basic/verify_7.6.0/designL12.tsen A basic/verify_7.6.0/designL20.tsen A basic/verify_7.6.0/designL21.tsen A basic/verify_7.6.0/designL22.tsen A basic/verify_7.6.0/designL30.tsen A basic/verify_7.6.0/designL31.tsen A basic/verify_7.6.0/designL32.tsen A basic/verify_7.6.0/designL33.tsen A basic/verify_7.6.0/designL34.tsen A basic/verify_7.6.0/designL40.tsen A basic/verify_7.6.0/designL41.tsen A basic/verify_7.6.0/designL42.tsen A basic/verify_7.6.0/design0c.gsen A basic/verify_7.6.0/design1b.tsen A basic/verify_7.6.0/design4.tsen A basic/verify_7.6.0/design8a.tsen A basic/verify_7.6.0/design8c.tsen A basic/verify_7.6.0/design8d.gsen A basic/verify_7.6.0/design8d.tsen A basic/verify_7.6.0/design9.gsen A basic/verify_7.6.0/designB4.tsen A basic/verify_7.6.0/designB5.tsen A basic/verify_7.6.0/designE4.gsen A basic/verify_7.6.0/designGB.tsen A basic/verify_7.6.0/designH3.tsen A basic/verify_7.6.0/designI1.tsen A basic/verify_7.6.0/designI2.tsen A basic/verify_7.6.0/designI3.tsen A basic/verify_7.6.0/designI4.tsen A basic/verify_7.6.0/designL31.gsen A basic/verify_7.6.0/designL32.gsen A basic/verify_7.6.0/designL33.gsen A basic/verify_7.6.0/designL34.gsen A basic/verify_7.6.0/designL41.gsen A basic/verify_7.6.0/designL42.gsen A basic/verify_7.6.0/designS3.tsen A basic/verify_7.6.0/designZ3.tsen A basic/verify_7.6.0/designZ4.tsen A basic/verify_7.6.0/designZ5.tsen A basic/verify_7.6.0/designZ6.gsen A basic/verify_7.6.0/designZ6.tsen A basic/verify_7.6.0/design0b.gsen A basic/verify_7.6.0/design0b.tsen A basic/verify_7.6.0/design0e.tsen A basic/verify_7.6.0/design0f.tsen A basic/verify_7.6.0/design0g.tsen A basic/verify_7.6.0/design0h.tsen A basic/verify_7.6.0/design0i.tsen A basic/verify_7.6.0/design0j.tsen A basic/verify_7.6.0/design0k.tsen A basic/verify_7.6.0/design0n1.tsen A basic/verify_7.6.0/design0n2.gsen A basic/verify_7.6.0/design0n2.tsen A basic/verify_7.6.0/design0o1.tsen A basic/verify_7.6.0/design0o2.gsen A basic/verify_7.6.0/design0o2.tsen A basic/verify_7.6.0/design0o3.tsen A 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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 A TRADES A TRADES/verify_7.8.0 A TRADES/verify_7.8.0/air1.vfy A TRADES/verify_7.8.0/air6.vfy A TRADES/verify_7.8.0/air_tile.vfy A TRADES/verify_7.8.0/demo1.vfy A TRADES/verify_7.8.0/demo2.vfy A TRADES/verify_7.8.0/demo3.vfy A TRADES/verify_7.8.0/demo3a.vfy A TRADES/verify_7.8.0/demo3b.vfy A TRADES/verify_7.8.0/demo_tile.vfy A TRADES/verify_7.8.0/hx0a.vfy A TRADES/verify_7.8.0/hx0b.vfy A TRADES/verify_7.8.0/hx1a.vfy A TRADES/verify_7.8.0/hx1b.vfy A TRADES/verify_7.8.0/hx2a.vfy A TRADES/verify_7.8.0/hx2b.vfy A TRADES/verify_7.8.0/hx3a.vfy A TRADES/verify_7.8.0/hx3b.vfy A TRADES/verify_7.8.0/hx4a.vfy A TRADES/verify_7.8.0/hx4b.vfy A TRADES/verify_7.8.0/hx_tile_a.vfy A TRADES/verify_7.8.0/hx_tile_b.vfy A TRADES/verify_7.8.0/liquid1.vfy A TRADES/verify_7.8.0/liquid6.vfy A TRADES/verify_7.8.0/liquid_tile.vfy A TRADES/verify_7.8.0/metal1.vfy A TRADES/verify_7.8.0/metal6.vfy A TRADES/verify_7.8.0/metal6_fig1.vfy A TRADES/verify_7.8.0/metal6_fig2.vfy A TRADES/verify_7.8.0/metal6_fig3.vfy A TRADES/verify_7.8.0/metal6_fig4.vfy A TRADES/verify_7.8.0/metal_tile.vfy A TRADES/verify_7.8.0/metal_tile_new.vfy A TRADES/verify_7.8.0/simple.vfy A TRADES/verify_7.8.0/simple_tile.vfy A TRADES/verify_7.8.0/tile1.vfy A TRADES/verify_7.8.0/tile2.vfy A TRADES/verify_7.8.0/tile3.vfy A TRADES/verify_7.8.0/tile4.vfy A TRADES/verify_7.8.0/tile5.vfy A TRADES/verify_7.8.0/tile6.vfy A TRADES/verify_7.8.0/tile_tile.vfy A TRADES/verify_7.7.0 A TRADES/verify_7.7.0/air1.vfy A TRADES/verify_7.7.0/air6.vfy A TRADES/verify_7.7.0/air_tile.vfy A TRADES/verify_7.7.0/demo1.vfy A TRADES/verify_7.7.0/demo2.vfy A TRADES/verify_7.7.0/demo3.vfy A TRADES/verify_7.7.0/demo3a.vfy A TRADES/verify_7.7.0/demo3b.vfy A TRADES/verify_7.7.0/demo_tile.vfy A TRADES/verify_7.7.0/hx0a.vfy A TRADES/verify_7.7.0/hx0b.vfy A TRADES/verify_7.7.0/hx1a.vfy A TRADES/verify_7.7.0/hx1b.vfy A TRADES/verify_7.7.0/hx2a.vfy A TRADES/verify_7.7.0/hx2b.vfy A TRADES/verify_7.7.0/hx3a.vfy A TRADES/verify_7.7.0/hx3b.vfy A TRADES/verify_7.7.0/hx4a.vfy A TRADES/verify_7.7.0/hx4b.vfy A TRADES/verify_7.7.0/hx_tile_a.vfy A TRADES/verify_7.7.0/hx_tile_b.vfy A TRADES/verify_7.7.0/liquid1.vfy A TRADES/verify_7.7.0/liquid6.vfy A TRADES/verify_7.7.0/liquid_tile.vfy A TRADES/verify_7.7.0/metal1.vfy A TRADES/verify_7.7.0/metal6.vfy A TRADES/verify_7.7.0/metal6_fig1.vfy A TRADES/verify_7.7.0/metal6_fig2.vfy A TRADES/verify_7.7.0/metal6_fig3.vfy A TRADES/verify_7.7.0/metal6_fig4.vfy A TRADES/verify_7.7.0/metal_tile.vfy A TRADES/verify_7.7.0/metal_tile_new.vfy A TRADES/verify_7.7.0/simple.vfy A TRADES/verify_7.7.0/simple_tile.vfy A TRADES/verify_7.7.0/tile1.vfy A TRADES/verify_7.7.0/tile2.vfy A TRADES/verify_7.7.0/tile3.vfy A TRADES/verify_7.7.0/tile4.vfy A TRADES/verify_7.7.0/tile5.vfy A TRADES/verify_7.7.0/tile6.vfy A TRADES/verify_7.7.0/tile_tile.vfy A TRADES/verify_7.6.0 A TRADES/verify_7.6.0/air1.vfy A TRADES/verify_7.6.0/air6.vfy A TRADES/verify_7.6.0/air_tile.vfy A TRADES/verify_7.6.0/demo1.vfy A TRADES/verify_7.6.0/demo2.vfy A TRADES/verify_7.6.0/demo3.vfy A TRADES/verify_7.6.0/demo3a.vfy A TRADES/verify_7.6.0/demo3b.vfy A TRADES/verify_7.6.0/demo_tile.vfy A TRADES/verify_7.6.0/hx0a.vfy A TRADES/verify_7.6.0/hx0b.vfy A TRADES/verify_7.6.0/hx1a.vfy A TRADES/verify_7.6.0/hx1b.vfy A TRADES/verify_7.6.0/hx2a.vfy A TRADES/verify_7.6.0/hx2b.vfy A TRADES/verify_7.6.0/hx3a.vfy A TRADES/verify_7.6.0/hx3b.vfy A TRADES/verify_7.6.0/hx4a.vfy A TRADES/verify_7.6.0/hx4b.vfy A TRADES/verify_7.6.0/hx_tile_a.vfy A TRADES/verify_7.6.0/hx_tile_b.vfy A TRADES/verify_7.6.0/liquid1.vfy A TRADES/verify_7.6.0/liquid6.vfy A TRADES/verify_7.6.0/liquid_tile.vfy A TRADES/verify_7.6.0/metal1.vfy A TRADES/verify_7.6.0/metal6.vfy A TRADES/verify_7.6.0/metal6_fig1.vfy A TRADES/verify_7.6.0/metal6_fig2.vfy A TRADES/verify_7.6.0/metal6_fig3.vfy A TRADES/verify_7.6.0/metal6_fig4.vfy A TRADES/verify_7.6.0/metal_tile.vfy A TRADES/verify_7.6.0/metal_tile_new.vfy A TRADES/verify_7.6.0/simple.vfy A TRADES/verify_7.6.0/simple_tile.vfy A TRADES/verify_7.6.0/tile1.vfy A TRADES/verify_7.6.0/tile2.vfy A TRADES/verify_7.6.0/tile3.vfy A TRADES/verify_7.6.0/tile4.vfy A TRADES/verify_7.6.0/tile5.vfy A TRADES/verify_7.6.0/tile6.vfy A TRADES/verify_7.6.0/tile_tile.vfy A TRADES/air1.csm A TRADES/air6.csm A TRADES/air_tile.csm A TRADES/demo1.csm A TRADES/demo2.csm A TRADES/demo3.csm A TRADES/demo3a.csm A TRADES/demo3b.csm A TRADES/demo_tile.csm A TRADES/hx0a.csm A TRADES/hx0b.csm A TRADES/hx1a.csm A TRADES/hx1b.csm A TRADES/hx2a.csm A TRADES/hx2b.csm A TRADES/hx3a.csm A TRADES/hx3b.csm A TRADES/hx4a.csm A TRADES/hx4b.csm A TRADES/hx_tile_a.csm A TRADES/hx_tile_b.csm A TRADES/liquid1.csm A TRADES/liquid6.csm A TRADES/liquid_tile.csm A TRADES/metal1.csm A TRADES/metal6.csm A TRADES/metal_tile.csm A TRADES/metal_tile_new.csm A TRADES/simple.csm A TRADES/tile1.csm A TRADES/tile2.csm A TRADES/tile3.csm A TRADES/tile4.csm A TRADES/tile5.csm A TRADES/tile6.csm A TRADES/tile_tile.csm A TRADES/metal6_fig1.csm A TRADES/metal6_fig2.csm A TRADES/metal6_fig3.csm A TRADES/metal6_fig4.csm A TRADES/simple_tile.csm A Tblade3 A Tblade3/Case7-28-8_IGV A Tblade3/Case7-28-8_IGV/verify_7.8.0 A Tblade3/Case7-28-8_IGV/verify_7.8.0/tblade_IGV.vfy A Tblade3/Case7-28-8_IGV/verify_7.7.0 A Tblade3/Case7-28-8_IGV/verify_7.7.0/tblade_IGV.vfy A Tblade3/Case7-28-8_IGV/verify_7.6.0 A Tblade3/Case7-28-8_IGV/verify_7.6.0/tblade_IGV.vfy A Tblade3/Case7-28-8_IGV/3dbgbinput.1.dat A Tblade3/Case7-28-8_IGV/README.txt A Tblade3/Case7-28-8_IGV/spancontrolinputs.1.dat A Tblade3/Case7-28-8_IGV/tblade_IGV.csm A Tblade3/Case7-28-8_OGV A Tblade3/Case7-28-8_OGV/verify_7.8.0 A Tblade3/Case7-28-8_OGV/verify_7.8.0/tblade_OGV.vfy A Tblade3/Case7-28-8_OGV/verify_7.7.0 A Tblade3/Case7-28-8_OGV/verify_7.7.0/tblade_OGV.vfy A Tblade3/Case7-28-8_OGV/verify_7.6.0 A Tblade3/Case7-28-8_OGV/verify_7.6.0/tblade_OGV.vfy A Tblade3/Case7-28-8_OGV/3dbgbinput.3.dat A Tblade3/Case7-28-8_OGV/README.txt A Tblade3/Case7-28-8_OGV/spancontrolinputs.3.dat A Tblade3/Case7-28-8_OGV/tblade_OGV.csm A Tblade3/Case7-28-8_Rotor A Tblade3/Case7-28-8_Rotor/tblade_rotor_flend.csm A Tblade3/Case7-28-8_Rotor/verify_7.8.0 A Tblade3/Case7-28-8_Rotor/verify_7.8.0/tblade_rotor.vfy A Tblade3/Case7-28-8_Rotor/verify_7.8.0/tblade_rotor_flend.vfy A Tblade3/Case7-28-8_Rotor/verify_7.8.0/tblade_rotor_hubwedge.vfy A Tblade3/Case7-28-8_Rotor/verify_7.7.0 A Tblade3/Case7-28-8_Rotor/verify_7.7.0/tblade_rotor.vfy A Tblade3/Case7-28-8_Rotor/verify_7.7.0/tblade_rotor_flend.vfy A Tblade3/Case7-28-8_Rotor/verify_7.7.0/tblade_rotor_hubwedge.vfy A Tblade3/Case7-28-8_Rotor/verify_7.6.0 A Tblade3/Case7-28-8_Rotor/verify_7.6.0/tblade_rotor.vfy A Tblade3/Case7-28-8_Rotor/verify_7.6.0/tblade_rotor_flend.vfy A Tblade3/Case7-28-8_Rotor/verify_7.6.0/tblade_rotor_hubwedge.vfy A Tblade3/Case7-28-8_Rotor/3dbgbinput.2.dat A Tblade3/Case7-28-8_Rotor/README.txt A Tblade3/Case7-28-8_Rotor/normalized_TE_derivative A Tblade3/Case7-28-8_Rotor/normalized_TE_derivative/3dbgbinput.2.dat A Tblade3/Case7-28-8_Rotor/normalized_TE_derivative/spancontrolinputs.2.dat A Tblade3/Case7-28-8_Rotor/spancontrolinputs.2.dat A Tblade3/Case7-28-8_Rotor/tblade_rotor.csm A Tblade3/Case7-28-8_Rotor/tblade_rotor_hubwedge.csm A Tblade3/Case9-22-1_Rotor A Tblade3/Case9-22-1_Rotor/verify_7.8.0 A Tblade3/Case9-22-1_Rotor/verify_7.8.0/tblade_rotor.vfy A Tblade3/Case9-22-1_Rotor/verify_7.7.0 A Tblade3/Case9-22-1_Rotor/verify_7.7.0/tblade_rotor.vfy A Tblade3/Case9-22-1_Rotor/verify_7.6.0 A Tblade3/Case9-22-1_Rotor/verify_7.6.0/tblade_rotor.vfy A Tblade3/Case9-22-1_Rotor/3dbgbinput.2.dat A Tblade3/Case9-22-1_Rotor/spancontrolinputs.2.dat A Tblade3/Case9-22-1_Rotor/tblade_rotor.csm A Tblade3/NACA_thickness A Tblade3/NACA_thickness/verify_7.8.0 A Tblade3/NACA_thickness/verify_7.8.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness/verify_7.8.0/tblade_NACA_thickness_dot.vfy A Tblade3/NACA_thickness/verify_7.7.0 A Tblade3/NACA_thickness/verify_7.7.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness/verify_7.7.0/tblade_NACA_thickness_dot.vfy A Tblade3/NACA_thickness/verify_7.6.0 A Tblade3/NACA_thickness/verify_7.6.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness/3dbgbinput.2.dat A Tblade3/NACA_thickness/README.txt A Tblade3/NACA_thickness/spancontrolinputs.2.dat A Tblade3/NACA_thickness/tblade_NACA_thickness.csm A Tblade3/NACA_thickness_with_derivative A Tblade3/NACA_thickness_with_derivative/verify_7.8.0 A Tblade3/NACA_thickness_with_derivative/verify_7.8.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness_with_derivative/verify_7.7.0 A Tblade3/NACA_thickness_with_derivative/verify_7.7.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness_with_derivative/verify_7.6.0 A Tblade3/NACA_thickness_with_derivative/verify_7.6.0/tblade_NACA_thickness.vfy A Tblade3/NACA_thickness_with_derivative/3dbgbinput.2.dat A Tblade3/NACA_thickness_with_derivative/README.txt A Tblade3/NACA_thickness_with_derivative/spancontrolinputs.2.dat A Tblade3/NACA_thickness_with_derivative/tblade_NACA_thickness.csm A Tblade3/Wennerstrom_with_umxthk A Tblade3/Wennerstrom_with_umxthk/verify_7.8.0 A Tblade3/Wennerstrom_with_umxthk/verify_7.7.0 A Tblade3/Wennerstrom_with_umxthk/verify_7.6.0 A Tblade3/Wennerstrom_with_umxthk/3dbgbinput.1.dat A Tblade3/Wennerstrom_with_umxthk/README.txt A Tblade3/Wennerstrom_with_umxthk/spancontrolinputs.1.dat A Tblade3/Wennerstrom_with_umxthk/tblade_Wennerstrom.csm_segfault A Tblade3/hub_inflation A Tblade3/hub_inflation/verify_7.8.0 A Tblade3/hub_inflation/verify_7.8.0/tblade_hub_inflation.vfy A Tblade3/hub_inflation/verify_7.8.0/tblade_hub_inflation_blade.vfy A Tblade3/hub_inflation/verify_7.7.0 A Tblade3/hub_inflation/verify_7.7.0/tblade_hub_inflation.vfy A Tblade3/hub_inflation/verify_7.7.0/tblade_hub_inflation_blade.vfy A Tblade3/hub_inflation/verify_7.6.0 A Tblade3/hub_inflation/verify_7.6.0/tblade_hub_inflation.vfy A Tblade3/hub_inflation/verify_7.6.0/tblade_hub_inflation_blade.vfy A Tblade3/hub_inflation/3dbgbinput.2.dat A Tblade3/hub_inflation/README.txt A Tblade3/hub_inflation/spancontrolinputs.2.dat A Tblade3/hub_inflation/tblade_hub_inflation.csm A Tblade3/hub_inflation/tblade_hub_inflation_blade.csm A Tblade3/hub_tip_inflation A Tblade3/hub_tip_inflation/verify_7.8.0 A Tblade3/hub_tip_inflation/verify_7.8.0/tblade_hub_tip_inflation.vfy A Tblade3/hub_tip_inflation/verify_7.8.0/tblade_hub_tip_inflation_blade.vfy A Tblade3/hub_tip_inflation/verify_7.7.0 A Tblade3/hub_tip_inflation/verify_7.7.0/tblade_hub_tip_inflation.vfy A Tblade3/hub_tip_inflation/verify_7.7.0/tblade_hub_tip_inflation_blade.vfy A Tblade3/hub_tip_inflation/verify_7.6.0 A Tblade3/hub_tip_inflation/verify_7.6.0/tblade_hub_tip_inflation.vfy A Tblade3/hub_tip_inflation/verify_7.6.0/tblade_hub_tip_inflation_blade.vfy A Tblade3/hub_tip_inflation/3dbgbinput.2.dat A Tblade3/hub_tip_inflation/README.txt A Tblade3/hub_tip_inflation/spancontrolinputs.2.dat A Tblade3/hub_tip_inflation/tblade_hub_tip_inflation.csm A Tblade3/hub_tip_inflation/tblade_hub_tip_inflation_blade.csm A Tblade3/tip_inflation A Tblade3/tip_inflation/verify_7.8.0 A Tblade3/tip_inflation/verify_7.8.0/tblade_tip_inflation.vfy A Tblade3/tip_inflation/verify_7.8.0/tblade_tip_inflation_blade.vfy A Tblade3/tip_inflation/verify_7.7.0 A Tblade3/tip_inflation/verify_7.7.0/tblade_tip_inflation.vfy A Tblade3/tip_inflation/verify_7.7.0/tblade_tip_inflation_blade.vfy A Tblade3/tip_inflation/verify_7.6.0 A Tblade3/tip_inflation/verify_7.6.0/tblade_tip_inflation.vfy A Tblade3/tip_inflation/verify_7.6.0/tblade_tip_inflation_blade.vfy A Tblade3/tip_inflation/3dbgbinput.2.dat A Tblade3/tip_inflation/README.txt A Tblade3/tip_inflation/spancontrolinputs.2.dat A Tblade3/tip_inflation/tblade_tip_inflation.csm A Tblade3/tip_inflation/tblade_tip_inflation_blade.csm A capsExamples A capsExamples/verify_7.8.0 A capsExamples/verify_7.8.0/transport.vfy A capsExamples/verify_7.8.0/transport.vfy_hand A capsExamples/verify_7.8.0/wing1.vfy A capsExamples/verify_7.8.0/wing1.vfy_hand A capsExamples/verify_7.8.0/wing2.vfy A capsExamples/verify_7.8.0/wing2.vfy_hand A capsExamples/verify_7.8.0/wing3.vfy A capsExamples/verify_7.8.0/wing3.vfy_hand A capsExamples/verify_7.8.0/wing4.vfy A capsExamples/verify_7.8.0/wing4.vfy_hand A capsExamples/verify_7.7.0 A capsExamples/verify_7.7.0/transport.vfy A capsExamples/verify_7.7.0/transport.vfy_hand A capsExamples/verify_7.7.0/wing1.vfy A capsExamples/verify_7.7.0/wing1.vfy_hand A capsExamples/verify_7.7.0/wing2.vfy A capsExamples/verify_7.7.0/wing2.vfy_hand A capsExamples/verify_7.7.0/wing3.vfy A capsExamples/verify_7.7.0/wing3.vfy_hand A capsExamples/verify_7.7.0/wing4.vfy A capsExamples/verify_7.7.0/wing4.vfy_hand A capsExamples/verify_7.6.0 A capsExamples/verify_7.6.0/transport.vfy A capsExamples/verify_7.6.0/transport.vfy_hand A capsExamples/verify_7.6.0/wing1.vfy A capsExamples/verify_7.6.0/wing1.vfy_hand A capsExamples/verify_7.6.0/wing2.vfy A capsExamples/verify_7.6.0/wing2.vfy_hand A capsExamples/verify_7.6.0/wing3.vfy A capsExamples/verify_7.6.0/wing3.vfy_hand A capsExamples/verify_7.6.0/wing4.vfy A capsExamples/verify_7.6.0/wing4.vfy_hand A capsExamples/transport.csm A capsExamples/wing1.csm A capsExamples/wing2.csm A capsExamples/wing3.csm A capsExamples/wing4.csm A capsExamples/wing4.jrnl A capsExamples/exercise_1_1.py A capsExamples/exercise_1_2.py A capsExamples/exercise_2_1.py A capsExamples/exercise_3_1.py A capsExamples/exercise_3_2.py A capsExamples/runAll.py A capsExamples/template_astrosModal.py A capsExamples/template_astrosStatic.py A capsExamples/template_dataTransfer.py A 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python/growing1.py A python/growing2.py A python/growing3.py A python/plotter1.py A python/plotter2.py A python/shapes.py A python/mitten2.py A python/test.py A python/mitten1.py A python/test1.py A python/test2.py A python/test3.py A python/growing.csm A python/test.csm A python/box.csm A python/cone.egads A python/cyl.csm A verify_7.7.0 A verify_7.7.0/CE13_LDI_Combustor_Test_Section_1.vfy A verify_7.7.0/CE13_LDI_Combustor_Test_Section_2.vfy A verify_7.7.0/CRM_NACA.vfy A verify_7.7.0/Carrera.vfy A verify_7.7.0/GEM_year1a.vfy A verify_7.7.0/GEM_year1b.vfy A verify_7.7.0/GEM_year1c.vfy A verify_7.7.0/GEM_year2.vfy A verify_7.7.0/M85_modified.vfy A verify_7.7.0/RM-10.vfy A verify_7.7.0/X29.vfy A verify_7.7.0/afrl_wing1.vfy A verify_7.7.0/afrl_wing2.vfy A verify_7.7.0/afrl_wing3.vfy A verify_7.7.0/bottle.vfy A verify_7.7.0/bottle2.vfy A verify_7.7.0/controlarm.vfy A verify_7.7.0/fighter1.vfy A verify_7.7.0/fighter2.vfy A verify_7.7.0/fighter3.vfy A verify_7.7.0/fighter4.vfy A verify_7.7.0/grc_nozzle1.vfy A verify_7.7.0/grc_nozzle9.vfy A verify_7.7.0/jmr3a.vfy A verify_7.7.0/jmr3b.vfy A verify_7.7.0/jsc_config1.vfy A verify_7.7.0/lander.vfy A verify_7.7.0/lander_leg.vfy A verify_7.7.0/partspanflap1.vfy A verify_7.7.0/partspanflap2.vfy A verify_7.7.0/spear0.vfy A verify_7.7.0/spear1.vfy A verify_7.7.0/tutorial1.vfy A verify_7.7.0/tutorial2.vfy A verify_7.7.0/tutorial3.vfy A verify_7.7.0/tutorial4.vfy A verify_7.7.0/tutorial5.vfy A verify_7.7.0/wingbody.vfy A ide AU compare760and741 A tutorial6 A tutorial6/stub.py A tutorial6/sizeWing.py A tutorial6/model2b.csm A tutorial6/model2c.csm A tutorial6/tutorial6.txt A tutorial6/bendWing.py A tutorial6/conserveUpper.py A tutorial6/interpolateUpper.py A tutorial6/model1.csm A tutorial6/model2a.csm A tutorial6/model3.csm A tutorial6/model4.csm A tutorial6/model5.csm A tutorial6/model5a.udc_orig A tutorial6/model5b.udc A tutorial6/optTaper.py A tutorial6/viewBodys.py A Gloves A Gloves/transport00.csm A Gloves/transport01.csm A Gloves/transport02.csm A Gloves/transport03.csm A Gloves/transport04.csm A verify_7.6.0 A verify_7.6.0/CE13_LDI_Combustor_Test_Section_1.vfy A verify_7.6.0/CE13_LDI_Combustor_Test_Section_2.vfy A verify_7.6.0/CRM_NACA.vfy A verify_7.6.0/Carrera.vfy A verify_7.6.0/GEM_year1a.vfy A verify_7.6.0/GEM_year1b.vfy A verify_7.6.0/GEM_year1c.vfy A verify_7.6.0/GEM_year2.vfy A verify_7.6.0/M85_modified.vfy A verify_7.6.0/RM-10.vfy A verify_7.6.0/X29.vfy A verify_7.6.0/afrl_wing1.vfy A verify_7.6.0/afrl_wing2.vfy A verify_7.6.0/afrl_wing3.vfy A verify_7.6.0/bottle.vfy A verify_7.6.0/bottle2.vfy A verify_7.6.0/controlarm.vfy A verify_7.6.0/fighter1.vfy A verify_7.6.0/fighter2.vfy A verify_7.6.0/fighter3.vfy A verify_7.6.0/fighter4.vfy A verify_7.6.0/grc_nozzle1.vfy A verify_7.6.0/grc_nozzle9.vfy A verify_7.6.0/jmr3a.vfy A verify_7.6.0/jmr3b.vfy A verify_7.6.0/jsc_config1.vfy A verify_7.6.0/lander.vfy A verify_7.6.0/lander_leg.vfy A verify_7.6.0/partspanflap1.vfy A verify_7.6.0/partspanflap2.vfy A verify_7.6.0/spear0.vfy A verify_7.6.0/spear1.vfy A verify_7.6.0/tutorial1.vfy A verify_7.6.0/tutorial2.vfy A verify_7.6.0/tutorial3.vfy A verify_7.6.0/tutorial4.vfy A verify_7.6.0/tutorial5.vfy A verify_7.6.0/wingbody.vfy A tutorial1.csm A tutorial4.csm A tutorial5.csm A tutorial2.csm A tutorial3.csm A tutorial_sketch1.udc A colors.dict A X29.csm A bottle.csm A bottle2.csm A CE13_LDI_Combustor_Test_Section_1.csm A Parka A Parka/block_combined.csm A Parka/block_in.csm A Parka/blockx_combined.csm A Parka/blockx_in.csm A Parka/blocky_combined.csm A Parka/blocky_in.csm A Parka/blockz_combined.csm A Parka/blockz_in.csm A Parka/parka1_combined.csm A Parka/parka1_in.csm A Parka/parka2_combined.csm A Parka/parka2_in.csm A CE13_LDI_Combustor_Test_Section_2.csm A CRM_NACA.csm A Carrera.csm A GEM_year2.csm A M85_modified.csm A RM-10.csm A afrl_wing1.csm A controlarm.csm A fighter2.csm A fun3d A fun3d/wingDemo.csm AU fun3d/fdsurf.py A fun3d/customDV.1 A fun3d/fun3d.nml A fun3d/rubber.data A fun3d/design.nml A fun3d/README A fun3d/command_line.options A fun3d/writeFiles.dict A fun3d/user_def_param_files.data A fun3d/wingDemo.mapbc AU fun3d/ocsm.sh A partspanflap1.csm A wingbody.csm A Carrera.dat A lander_leg.dat A lander.dat A jmr3a.dat A jmr3b.dat A GEM_year1.jnl AU GEM_year1_sketches.pdf A CE13_LDI_Combustor_Test_Section_1.STEP A CE13_LDI_Combustor_Test_Section_2.STEP U . At revision 2476 Checking out a fresh workspace because /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/pyOCSM doesn't exist Cleaning local Directory OpenCSM/trunk/pyOCSM Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-04-09T22:19:08.826 -0400' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A pyOCSM A pyOCSM/ocsm.py A pyOCSM/esp.py A pyOCSM/__init__.py A testOCSM A testOCSM/test_pyOCSM.py A testOCSM/inline.csm A testOCSM/sample.csm A testOCSM/sample.dict U . At revision 2476 Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP 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/udc since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [viggen] is in [[macys, macys_VM, reynolds, viggen]] Run condition [Execution node ] enabling perform for step [Execute shell] [DARWIN_ARM64] $ /bin/bash -xe /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins17670007473334600536.sh + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training/lectures + [[ CAPS/LINEARAERO != *\S\l\u\g\s* ]] + rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/data/Slugs + [[ viggen == *\v\i\g\g\e\n* ]] + arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/JenkinsESP/ESP_Regression.sh + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 ++ [[ viggen == \r\e\y\n\o\l\d\s ]] ++ [[ DARWIN_ARM64 == *\.\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 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64 ++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/julia ++ export AWAVE=awavemod.f ++ AWAVE=awavemod.f ++ export RLM_CONNECT_TIMEOUT=350 ++ RLM_CONNECT_TIMEOUT=350 ++ [[ 7.6 != '' ]] ++ [[ '' != '' ]] ++ [[ viggen == *\r\e\y\n\o\l\d\s* ]] ++ [[ viggen == *\m\a\c\y\s* ]] ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export EMPnumProc=2 ++ EMPnumProc=2 ++ export OMP_NUM_THREADS=2 ++ OMP_NUM_THREADS=2 ++ source /Users/jenkins/.bash_profile ++++ /opt/homebrew/bin/brew shellenv +++ eval 'export HOMEBREW_PREFIX="/opt/homebrew"; export HOMEBREW_CELLAR="/opt/homebrew/Cellar"; export HOMEBREW_REPOSITORY="/opt/homebrew"; export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}"; export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:"; export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";' ++++ export HOMEBREW_PREFIX=/opt/homebrew ++++ HOMEBREW_PREFIX=/opt/homebrew ++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar ++++ export HOMEBREW_REPOSITORY=/opt/homebrew ++++ HOMEBREW_REPOSITORY=/opt/homebrew ++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin ++++ export MANPATH=/opt/homebrew/share/man: ++++ MANPATH=/opt/homebrew/share/man: ++++ export INFOPATH=/opt/homebrew/share/info: ++++ INFOPATH=/opt/homebrew/share/info: +++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]] +++ . /opt/homebrew/etc/profile.d/bash_completion.sh ++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']' ++++ return ++ [[ viggen == *\m\a\c\y\s* ]] ++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \m\a\c\y\s ]] ++ export CASARCH=. ++ CASARCH=. ++ '[' '!' -z '' ']' +++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ CASROOT=/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 ++ export UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/udunits/udunits2.xml ++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib ++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9 ++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.9 ++ [[ viggen == *\m\a\c\y\s* ]] ++ export AFLR_ARCH=MacOSX-arm64 ++ AFLR_ARCH=MacOSX-arm64 ++ 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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/ ++ [[ viggen == \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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/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:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']' +++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl ++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH; PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB; PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT; PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT; PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;' +++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 +++ export PERL5LIB +++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_LOCAL_LIB_ROOT +++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"' +++ export PERL_MB_OPT +++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl +++ export PERL_MM_OPT ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin ++ [[ viggen == \m\a\c\y\s* ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*' ++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv +++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-build /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-c++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/analyze-cc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-build /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-c++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++ ++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`' +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc +++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc ++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/bin/intercept-cc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc +++ python-config --includes ++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11' ++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11' +++ python-config --help ++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]] +++ python-config --ldflags --embed ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation' ++ [[ viggen == \m\a\c\y\s ]] ++ [[ viggen == \v\i\g\g\e\n ]] ++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w' ++ export PYTHONUNBUFFERED=true ++ PYTHONUNBUFFERED=true ++ export PYTHONFAULTHANDLER=true ++ PYTHONFAULTHANDLER=true ++ python --version Python 3.11.6 ++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]] ++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/data ++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/data + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/JenkinsESP/ESPbfr.sh ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ ++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv created virtual environment CPython3.11.6.final.0-64 in 261ms creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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==69.1.1, wheel==0.43.0 activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator ++ . /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/activate +++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv +++ '[' darwin23 = cygwin ']' +++ '[' darwin23 = msys ']' +++ export VIRTUAL_ENV +++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin +++ export PATH +++ '[' x '!=' x ']' ++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy Collecting numpy Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB) Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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-1.13.0-cp311-cp311-macosx_12_0_arm64.whl.metadata (60 kB) Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (1.26.4) Using cached scipy-1.13.0-cp311-cp311-macosx_12_0_arm64.whl (30.3 MB) Installing collected packages: scipy Successfully installed scipy-1.13.0 ++ pip_install openmdao ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao Collecting openmdao Using cached openmdao-3.31.1-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB) Requirement already satisfied: numpy 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) (1.13.0) 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-24.0-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_11_0_arm64.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-3.3-py3-none-any.whl (1.7 MB) Using cached packaging-24.0-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_11_0_arm64.whl (118 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-3.3 openmdao-3.31.1 packaging-24.0 requests-2.31.0 urllib3-2.2.1 ++ [[ viggen == *\v\i\g\g\e\n* ]] ++ export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib ++ CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib ++ export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 ++ CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0 ++ GCC_MAJOR=12 ++ export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a' ++ CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a' ++ pip_install cvxopt ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl.metadata (1.3 kB) Using cached cvxopt-1.3.2-cp311-cp311-macosx_11_0_arm64.whl (11.1 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 ++ pip_install dill ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging Requirement already satisfied: packaging in ./ESP/venv/lib/python3.11/site-packages (24.0) ++ pip_install matplotlib ++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib Collecting matplotlib Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (5.8 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.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-4.51.0-cp311-cp311-macosx_10_9_universal2.whl.metadata (159 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl.metadata (6.4 kB) Requirement already satisfied: numpy>=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) (24.0) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl.metadata (9.2 kB) Collecting pyparsing>=2.3.1 (from matplotlib) Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB) Collecting python-dateutil>=2.7 (from matplotlib) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB) Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib) Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB) Using cached matplotlib-3.8.4-cp311-cp311-macosx_11_0_arm64.whl (7.5 MB) Using cached contourpy-1.2.1-cp311-cp311-macosx_11_0_arm64.whl (245 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.51.0-cp311-cp311-macosx_10_9_universal2.whl (2.8 MB) Using cached kiwisolver-1.4.5-cp311-cp311-macosx_11_0_arm64.whl (66 kB) Using cached pillow-10.3.0-cp311-cp311-macosx_11_0_arm64.whl (3.4 MB) Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.51.0 kiwisolver-1.4.5 matplotlib-3.8.4 pillow-10.3.0 pyparsing-3.1.2 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/src ++ make touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64 touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Lazy.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Trad.h mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/always_inline.h clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsGeom.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsHLevel.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTopo.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsCopy.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsCopy.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSpline.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsIO.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsIO.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSplineFit.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSplineFit.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsSkinning.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSkinning.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \ -I. egadsTessSens.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessSens.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BRepLib_FuseEdges.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsFit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsRobust.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSBO.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmCfit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmGrid.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsExport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \ -I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSolids.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/emp.o clang++ -g -target arm64-apple-darwin -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 -ffp-model=strict -DREVISION=7.8 -IOCC -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaluate.o clang++ -g -target arm64-apple-darwin -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 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \ ../util/rational.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rational.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/Users/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/regQuads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1 SurrealD1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4 SurrealD4_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1 SurrealS1_test_suite Complete! clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4 SurrealS4_test_suite Complete! /Library/Developer/CommandLineTools/usr/bin/make -C ../util clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapFindUV.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapGen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapStructFree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapTest.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_add.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_bnd_adj.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_area_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_edge_ratio.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_cpu_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_find_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_from_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibeibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfibf.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccin.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_idibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inibe.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inl_uv_bnd.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_malloc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_mben_disc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_message.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_norm_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_solve.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_struct_tasks.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_test.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_to_egads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_version.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -lc++ \ -install_name '@rpath/libegads.dylib' \ -compatibility_version 7.8 \ -current_version 1.0.25 ) touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a cp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; \ ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsHLevel.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTopo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a emp.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a *** EGADS Build Complete! *** ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/wvServer ++ make clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/map.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/base64-decode.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/client-handshake.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libwebsockets.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-deflate-stream.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/md5.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-x-google-mux.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsers.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sha-1.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/server.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/wv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/browserMessage.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o; ) ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a \ -lpthread -lz -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 7.8 \ -current_version 1.0.25 ) ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/lite ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteMemory.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteGeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTopo.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteAttrs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteImport.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \ liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteString.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTris.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \ ../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTessInp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ratLite.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \ ../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteRegQuads.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ ../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteEffect.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \ -I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteUVmap.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include BSplineIGES.c -o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f CSys.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f GBO.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f SBO.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f addKnots.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f agglom.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f blend.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f chamfer.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f closure.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \ -legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f edge2WB.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f edges.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f effective.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include effective.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2cart.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cart.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egads2ply.make clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. egads2ply.cpp -std=c++11 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I. tinyply.cpp -std=c++11 -w \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsGeom_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsHLevel_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsSpline_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f egadsTopo_dot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f exportLite.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../util/uvmap \ ../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o -DSTANDALONE clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f extrot.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fillet.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fit.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fitTri.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fullAttr.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f fuseSheets.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f globalTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollow.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f hollowFace.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f intersect.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeCone.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeFace3D.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeFace3D.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f makeLoop.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mapTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mofb.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f mssb.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f multiContext.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include multiContext.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f offset.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f rebuild.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f refObj.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f replace.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f revolve.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f ruled.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f saveTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include saveTess.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f scribe.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f sew.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f simplePer.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include simplePer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f smallEdges.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include smallEdges.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f step.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f sweep.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f test.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f tolerance.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ for file in '`ls *.make`' ++ make -f union.make gfortran -g -c -O -frecursive -fcray-pointer -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \ -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w ++ for file in '`ls *.make`' ++ make -f vAttr.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vCurvature.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vEffect.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vEto.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vFrame.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vGeom.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vQuad.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver \ -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vTess.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include ../util/retessFaces.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet \ -lpthread -lz -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f vTessInp.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ for file in '`ls *.make`' ++ make -f xform.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/docs/Tutorial ++ make -f tire.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include tire.c clang++ -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ make -f egads2tri.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2tri.c clang++ -g -target arm64-apple-darwin -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o clang -g -target arm64-apple-darwin -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o clang -g -target arm64-apple-darwin -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o clang -g -target arm64-apple-darwin -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o clang -g -target arm64-apple-darwin -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/src ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -install_name '@rpath/libocsm.dylib' -compatibility_version 1.0.25 -current_version 1.0.25 clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWarp.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/EGADS/trunk/docs/UDP_UDF/data ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c -o tire.o clang -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c touch tire.so rm tire.so clang -g -target arm64-apple-darwin -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib ++ [[ '' == '' ]] ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS ++ make (cd src; make) touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \ -I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include \ -I/usr/include/udunits2 aimTransferUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \ aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBase.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAnalysis.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsApprox.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAttr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBound.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsProblem.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsValue.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsUnits.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/conjGrad.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsFunIDs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsChkInpt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \ -I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/printObject.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so: No such file or directory make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so] Error 1 (ignored) clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include phaseUtil.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm (cd aim; make) /Library/Developer/CommandLineTools/usr/bin/make -C utils clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/attrUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/meshUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cfdUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/feaUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/arrayUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/deprecateUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cardUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranCards.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jsonUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranOP2Reader.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmSpanSpace.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/arrayUtils.h cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrTypes.h cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrUtils.h cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardTypes.h cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardUtils.h cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdTypes.h cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdUtils.h cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/deprecateUtils.h cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaTypes.h cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaUtils.h cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/jsonUtils.h cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshTypes.h cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshUtils.h cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscTypes.h cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscUtils.h cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranCards.h cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranUtils.h cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/tecplotUtils.h cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmSpanSpace.h cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmTypes.h cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmUtils.h /Library/Developer/CommandLineTools/usr/bin/make -C abaqus clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o echo "Building Abaqus with Python" Building Abaqus with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib /Library/Developer/CommandLineTools/usr/bin/make -C aflr2 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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-arm64/lib -laflr2c -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-arm64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr3 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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-arm64/lib -laflr3 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version 16.32.49 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-arm64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C aflr4 clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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-arm64/lib -laflr4 -lm \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src -I../utils aflr4AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.9/src \ -I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.9/MacOSX-arm64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -lm /Library/Developer/CommandLineTools/usr/bin/make -C astros clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosCards.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C avl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \ -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C awave clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils awaveAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C cart3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \ cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \ writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D \ surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \ `xml2-config --cflags` ./xddm/xddm.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \ -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ \ -lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include cart3dTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I./xddm \ -I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ -lc3dio -lCart3D \ -lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm /Library/Developer/CommandLineTools/usr/bin/make -C cbaero clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o clang -g -target arm64-apple-darwin -bundle /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C cgt clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cgt.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include aflr4egads.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cgt /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl /Library/Developer/CommandLineTools/usr/bin/make -C custom make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C delaundo clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils delaundoAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C egadsTess clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils egadsTessAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C friction clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils frictionAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C fun3d clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \ fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \ -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o Building FUN3D with Python clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib /Library/Developer/CommandLineTools/usr/bin/make -C hsm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAdj.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.8 \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sbsolve.o /Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/genrcmi.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C interference clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. cloudFns.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C jfd3 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils jfd3AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/jfd3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C masstran clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils masstranAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C meshWriter /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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fastWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C libMeshbWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include libMeshbWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libMeshbWriter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include libMeshb/sources/libmeshb7.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libMeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libMeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C su2Writer clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include su2Writer.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C ugridWriter clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include ugridWriter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C mses clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C mystran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranUtils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C nastran clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils nastranAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C plato Not compiling platoAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C pointwise clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils pointwiseAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hashElement.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -lpthread /Library/Developer/CommandLineTools/usr/bin/make -C refine clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/libMeshbWriter refineAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C sierraSD Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C sierraSM Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment.... /Library/Developer/CommandLineTools/usr/bin/make -C skeleton clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils skeletonAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C spinnaker make[2]: Nothing to be done for `default'. /Library/Developer/CommandLineTools/usr/bin/make -C su2 clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2Utils.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_4_Cardinal.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_5_Raven.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_6_Falcon.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_7_Blackbird.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_8_Harrier.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_8_Harrier.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_8_Harrier.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C tacs clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tacsAIM.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w /Library/Developer/CommandLineTools/usr/bin/make -C tetgen clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tetgenAIM.cpp \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \ -DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o clang++ -g -target arm64-apple-darwin -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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o clang++ -g -target arm64-apple-darwin -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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \ -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm /Library/Developer/CommandLineTools/usr/bin/make -C tsfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm /Library/Developer/CommandLineTools/usr/bin/make -C unitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS cp -p -f pyCAPS/test_aflr2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr2.py cp -p -f pyCAPS/test_aflr3.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr3.py cp -p -f pyCAPS/test_aflr4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr4.py cp -p -f pyCAPS/test_astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_astros.py cp -p -f pyCAPS/test_avl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_avl.py cp -p -f pyCAPS/test_cart3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cart3d.py cp -p -f pyCAPS/test_cbaero.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cbaero.py cp -p -f pyCAPS/test_egadsTess.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_egadsTess.py cp -p -f pyCAPS/test_fun3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_fun3d.py cp -p -f pyCAPS/test_masstran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_masstran.py cp -p -f pyCAPS/test_mses.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_mses.py cp -p -f pyCAPS/test_pointwise.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_pointwise.py cp -p -f pyCAPS/test_refine.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_refine.py cp -p -f pyCAPS/test_su2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_su2.py cp -p -f pyCAPS/test_tacs.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tacs.py cp -p -f pyCAPS/test_tetgen.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tetgen.py cp -p -f pyCAPS/test_xfoil.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_xfoil.py cp -p -f pyCAPS/Makefile /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/Makefile mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/airfoilSection.csm cp -p -f csmData/avlSections.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/avlSections.csm cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfd2D.csm cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdMultiBody.csm cp -p -f csmData/cfdSingleBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdSingleBody.csm cp -p -f csmData/cornerGeom.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cornerGeom.csm cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaSimplePlate.csm cp -p -f csmData/feaWingOMLAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaWingOMLAero.csm cp -p -f csmData/kulfanSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSection.csm cp -p -f csmData/kulfanSymmetricSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSymmetricSection.csm cp -p -f csmData/masstran.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/masstran.csm cp -p -f csmData/multiRegions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/multiRegions.csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/cCAPS /Library/Developer/CommandLineTools/usr/bin/make -C xfoil clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \ xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm (cd Slugs/src; make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Fitter.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. RedBlackTree.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Tessellate.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o \ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \ -lpthread -lz -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \ -lpthread -lz -lm (cd test; make -f aim.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib cp -p -f testingAIM.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testingAIM.csm (cd test; make -f autoExec.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm \ -legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lz -lm -ldl (cd test; make -f newPhase.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \ -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f basic.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f geomIn.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (cd test; make -f utilsTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads \ -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl (cd test; make -f vVS.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib (cd examples; make) mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_AGARD445_PyTest.py cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr2_PyTest.py cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Generic_Missile.py cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_PyTest.py cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_TipTreat_PyTest.py cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_AGARD445_PyTest.py cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Aeroelastic_PyTest.py cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Composite_PyTest.py cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Flutter_15degree.py cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_OptControl_PyTest.py cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_PyTest.py cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBar_PyTest.py cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Trim_15degree.py cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/autoLink_Pytest.py cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_AutoSpan_PyTest.py cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_ControlSurf_PyTest.py cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_DesignSweep_PyTest.py cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_EigenValue_PyTest.py cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_PyTest.py cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/awave_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_PyTest.py cp -p -f pyCAPS/cbaero_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cbaero_PyTest.py cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/delaundo_PyTest.py cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_PyTest.py cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/friction_PyTest.py cp -p -f 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/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_refine_PyTest.py cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_AGARD445_PyTest.py cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_PyTest.py cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_PyTest.py cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_AGARD445_PyTest.py cp -p -f 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/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/tiptreat.csm cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.udc mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/boydBox.py cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/gp.py cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_blackbox.py cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_gp.py cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/qp.py cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/sp.py cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing1.csm cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing2.csm cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm/naca.csm cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Camber.py cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/MSES.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_CTestRegression.sh cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_PyTestRegression.sh (make -C cCAPS -f aeroelastic_SU2.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f avlTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f awaveTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f frictionTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f fun3d.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f hsm.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f interferenceTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceTest.c \ -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f msesTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f mystran.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o \ -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl (make -C cCAPS -f pointwiseTest.make) clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \ -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl +++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training/ -name Makefile ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//2023/data/session01 ++ make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl ++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`' ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]] +++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//data/session01/Makefile ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/training//data/session01 ++ make make: Nothing to be done for `default'. ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/src ++ make -f serveESP.make clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib ++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64 +++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/OpenCSM/trunk/data/training/ -name Makefile + mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/test + cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/test + source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/JenkinsESP/RunRegression.sh ++ [[ 0 == 1 ]] ++ [[ 0 == 2 ]] ++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64 == '' ]] ++ [[ CAPS/LINEARAERO == '' ]] ++ [[ 7.8 == '' ]] ++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/examples/ ++ make test TYPE=LINEARAERO (make -C cCAPS -f aeroelastic_SU2.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date. (make -C cCAPS -f avlTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest' is up to date. (make -C cCAPS -f awaveTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest' is up to date. (make -C cCAPS -f frictionTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest' is up to date. (make -C cCAPS -f msesTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest' is up to date. (make -C cCAPS -f mystran.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest' is up to date. (make -C cCAPS -f pointwiseTest.make) make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest' is up to date. (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_CTestRegression.sh LINEARAERO) Running.... LINEARAERO c-Tests ================================================= + echo './avlTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./avlTest test; + ./avlTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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":[1.751976980130e-01,4.816388142977e-01,7.134545983421e-01,8.955798774849e-01,1.045275116632e+00,1.165642609065e+00,1.251488483105e+00,1.294909342036e+00,1.290147495293e+00,1.237589733954e+00,1.147354354589e+00,1.069716379937e+00,1.027204841579e+00,9.123069911134e-01,8.271224835183e-01,7.465072383823e-01,6.622506856520e-01,5.718077594714e-01,4.773770050899e-01,3.839108464450e-01,2.965810831876e-01,2.166269422077e-01,1.372747954615e-01,4.847522879848e-02],"ai":[2.423376448059e-01,1.891573605669e-01,1.387726073609e-01,1.136377561110e-01,1.056109957987e-01,1.077519869781e-01,1.163918473303e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870070e-02,-4.190817556553e-02,-1.699095118257e-02,-7.589503463777e-04,7.958849673277e-03,1.019416065188e-02,8.688915578617e-03,6.053380335312e-03,5.120395026966e-03,9.296755297777e-03,2.004804046056e-02,3.330492577563e-02],"cl_norm":[2.044051829731e-01,5.494672225940e-01,7.808579037666e-01,9.268407130704e-01,1.014078158135e+00,1.057019341175e+00,1.062951411331e+00,1.036333388587e+00,9.816462634652e-01,9.051794884118e-01,8.167547094730e-01,7.499676468296e-01,7.211772113978e-01,6.503467495436e-01,6.057660560785e-01,5.686988847404e-01,5.305932247981e-01,4.861412346267e-01,4.332732553833e-01,3.727603475166e-01,3.071901673655e-01,2.373206031154e-01,1.568074209165e-01,5.666485024183e-02],"cl":[1.803741931755e-01,4.848688546456e-01,6.890559834541e-01,8.178762563193e-01,8.948575908400e-01,9.327503738518e-01,9.379850374383e-01,9.144963748396e-01,8.662385668547e-01,7.987616435479e-01,7.207325646086e-01,6.617973538491e-01,6.363916792637e-01,5.738884333901e-01,5.345488897542e-01,5.018395375442e-01,4.682137871228e-01,4.289878157184e-01,3.823352848865e-01,3.289366049978e-01,2.710752133780e-01,2.094198967377e-01,1.383722840114e-01,5.000302093674e-02],"cd":[4.708816796009e-03,1.893013552459e-02,2.388458719214e-02,2.809788812558e-02,3.450496926229e-02,4.310977683932e-02,5.296690620746e-02,6.273588035903e-02,7.092746653689e-02,7.623132904844e-02,7.793919402367e-02,1.330641046360e-01,7.642533954135e-02,1.575280561792e-02,1.020926164298e-02,5.734996040024e-03,2.453990236867e-03,7.034156943368e-05,-1.681061755703e-03,-2.904871637690e-03,-3.696799546923e-03,-4.291551637880e-03,-4.755989795801e-03,-4.178738547363e-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":[-6.175122770628e-02,-1.541367450247e-01,-1.990020049076e-01,-2.179523703797e-01,-2.259241555999e-01,-2.291785023831e-01,-2.301045091167e-01,-2.293937884748e-01,-2.266765134793e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694970e-01,-1.141869860843e-01,-1.128288355903e-01,-1.117855412668e-01,-1.094863434131e-01,-1.016126232938e-01,-7.889656776595e-02,-3.215621313953e-02],"cm_LE":[-9.907391078322e-02,-2.553625521059e-01,-3.443180862959e-01,-3.917771248733e-01,-4.170475207534e-01,-4.288879437377e-01,-4.309998082913e-01,-4.249313258857e-01,-4.112512348867e-01,-3.899661415021e-01,-3.610798550198e-01,-3.345295675167e-01,-3.190696575593e-01,-2.776668920569e-01,-2.496150543392e-01,-2.306580335185e-01,-2.170714278266e-01,-2.053105443163e-01,-1.932221818516e-01,-1.798625218872e-01,-1.643057066256e-01,-1.427050164897e-01,-1.051753523062e-01,-4.137433282272e-02],"C.P.x/c":[5.923506801009e-01,5.678936810396e-01,5.388038268096e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888068e-01,5.008416597224e-01,5.116790825908e-01,5.261470832206e-01,5.398832002652e-01,5.443357803973e-01,5.402488831883e-01,5.217174153488e-01,5.035437183301e-01,4.956552889214e-01,4.999897967898e-01,5.161776906019e-01,5.451044281037e-01,5.898391652627e-01,6.538965497759e-01,7.352099770688e-01,8.201760893059e-01,8.930854083839e-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":[4.143502484419e-02,1.146121890397e-01,1.669674480705e-01,2.000258625576e-01,2.165069436650e-01,2.173612378317e-01,2.020982864242e-01,1.687203348327e-01,1.143884794131e-01,4.073751989365e-02],"ai":[2.065296924523e-01,1.849180223915e-01,1.591285664757e-01,1.456224964408e-01,1.435231644007e-01,1.506386553621e-01,1.666466052407e-01,1.914179167695e-01,2.193221173430e-01,2.365321328633e-01],"cl_norm":[6.579957348177e-02,1.763463053601e-01,2.425545992662e-01,2.698370559986e-01,2.694590983040e-01,2.501591871290e-01,2.170544160382e-01,1.714623014106e-01,1.118766125250e-01,3.907064104111e-02],"cl":[5.682537081790e-02,1.522949719002e-01,2.094733190134e-01,2.330348048803e-01,2.327083956801e-01,2.160407403863e-01,1.874510278163e-01,1.480770823179e-01,9.661810337338e-02,3.374191575678e-02],"cd":[4.670566079260e-03,1.374698956983e-02,1.845844898552e-02,2.032218684725e-02,2.072187092673e-02,2.023884851599e-02,1.896705322934e-02,1.657142171121e-02,1.222733795468e-02,5.106244760924e-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":[-3.303465544544e-02,-8.761746958838e-02,-1.194746602282e-01,-1.341488123563e-01,-1.380350789963e-01,-1.339349413680e-01,-1.218867053325e-01,-1.002593790936e-01,-6.716156843032e-02,-2.373448304337e-02],"cm_LE":[-4.232877133357e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490116e-01,-1.757829360724e-01,-1.683239687784e-01,-1.510824211718e-01,-1.228726806389e-01,-8.171902803731e-02,-2.878672165377e-02],"C.P.x/c":[8.313363814431e-01,8.253142634661e-01,8.203574125378e-01,8.256599853193e-01,8.431675932569e-01,8.699522420101e-01,9.002322593392e-01,9.270755982234e-01,9.451240614895e-01,9.534124326091e-01]} real 0m1.581s user 0m0.372s sys 0m0.110s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./avlTest passed (as expected) ============================================= ================================================= + echo './msesTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./msesTest test; + ./msesTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm Value of CL = 0.276892 real 0m2.632s user 0m1.730s sys 0m0.086s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./msesTest passed (as expected) ============================================= ================================================= + echo './awaveTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./awaveTest test; + ./awaveTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.635s user 0m0.329s sys 0m0.043s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./awaveTest passed (as expected) ============================================= ================================================= + echo './frictionTest test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt ./frictionTest test; + ./frictionTest 0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/cCAPSlog.txt Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default). Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Running FRICTION! Value of CDfric = 0.009900 Value of CDfric = 0.009190 real 0m0.416s user 0m0.197s sys 0m0.039s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./frictionTest passed (as expected) ============================================= All tests pass! ================================================= ================================================= (cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest; ./execute_PyTestRegression.sh LINEARAERO) ================================================= Using python : /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... LINEARAERO PyTests avl: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/avl ================================================= + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0.0006119078685800925 CYtot -6.292592518559147e-15 CZtot -0.3012861394881712 Cltot -4.783069014642483e-14 Cmtot -0.1945055953448147 Cntot -2.338890054396671e-15 Cl'tot -4.786422456048383e-14 Cn'tot -1.50377318550154e-15 CLtot 0.3012509314146395 CDtot 0.00464635348821979 CDvis 0.0 CLff 0.3009503023516151 CYff -7.7198870803959e-15 CDind 0.00464635348821979 CDff 0.004968969500894849 e 0.9669902146155998 StripForces Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407] Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453] real 0m2.298s user 0m0.886s sys 0m0.254s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -0.04120015660053111 CYtot 2.462543613195682e-10 CZtot -1.125018850856348 Cltot 1.184580814522611e-09 Cmtot -1.954741252395341 Cntot -1.790133030044494e-10 Cl'tot 1.181276184205198e-09 Cn'tot -1.996598242441884e-10 CLtot 1.124128463157939 CDtot 0.06082816785187402 CDvis 0.0 CLff 1.123105484603622 CYff 2.611430934031642e-10 CDind 0.06082816785187402 CDff -0.2032104788139517 e -0.3293015989519321 real 0m9.579s user 0m8.206s sys 0m4.247s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 Cl[0] = 0.2009337808873524 Cd[0] = 0.002572533601550775 real 0m35.611s user 0m12.854s sys 0m12.716s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -0.01911479917641001 CYtot 0.03828770401115553 CZtot -0.6203123021537938 Cltot 0.05803020542928473 Cmtot -0.3649415791575079 Cntot -0.02051317548232544 Cl'tot 0.05766336287208538 Cn'tot -0.02152281795713262 CLtot 0.6198842263414319 CDtot 0.02993783031514586 CDvis 0.0 CLff 0.6192452092592853 CYff 0.03287079625844261 CDind 0.02993783031514586 CDff 0.0286101982265777 e 0.7130586920543264 real 0m0.959s user 0m0.820s sys 0m0.277s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected) ================================================= ================================================= + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt + echo 'avl_EigenValue_PyTest.py test;' avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.867s user 0m0.666s sys 0m0.244s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 [3.72334444e-08] Cmtot2_Alpha [[0.00055304]] Cmtot2_Beta [[8.73257587e-06]] At iterate 4 f= 3.72334D-08 |proj g|= 5.53036D-04 Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.19764419e-12] Cmtot2_Alpha [[4.24792989e-06]] Cmtot2_Beta [[6.7141843e-08]] At iterate 5 f= 2.19764D-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 = 2.1976441939068914E-012 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-5.50424967] [2.89504288] real 0m7.491s user 0m2.605s sys 0m0.803s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected) ================================================= awave: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/awave ================================================= + echo 'awave_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = [1.13333237, 0.216380283] real 0m0.639s user 0m0.769s sys 0m0.108s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected) ================================================= friction: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/friction ================================================= + echo 'friction_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.518s user 0m0.577s sys 0m0.105s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt tsfoil_PyTest.py test; + python -u tsfoil_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Getting results PAUSE Press the ENTER key to exit To resume execution, type go. Other input will terminate the job. Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG Cl = 0.933407 Cd = 0.000284 Cd Wave = 0.0 Cm = -0.203436 Cp _Critcal = -1.303869 real 0m0.546s user 0m0.617s sys 0m0.092s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected) ================================================= mses: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/mses ================================================= + echo 'mses_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Cl = 0.3783791085548177 Cd = 0.007775858417209677 Cm = 0.005262636995835036 real 0m3.525s user 0m3.050s sys 0m0.168s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 [[0.1764758]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 1 M = 10 At X0 1 variables are exactly at the bounds At iterate 0 f= 1.32653D-02 |proj g|= 1.76476D-01 camber [-0.0764758] CD [0.01022332] CD_camber [[-0.08759853]] At iterate 1 f= 1.02233D-02 |proj g|= 8.75985D-02 camber [-0.01793539] CD [0.00770373] CD_camber [[-0.01328932]] At iterate 2 f= 7.70373D-03 |proj g|= 1.32893D-02 camber [-0.00746613] CD [0.00760241] CD_camber [[-0.00542337]] At iterate 3 f= 7.60241D-03 |proj g|= 5.42337D-03 camber [-0.00024784] CD [0.00758207] CD_camber [[-0.00011854]] At iterate 4 f= 7.58207D-03 |proj g|= 1.18538D-04 camber [-8.65457493e-05] CD [0.00758207] CD_camber [[-3.94469721e-06]] camber [-0.00019629] CD [0.00758207] CD_camber [[-8.4257979e-05]] At iterate 5 f= 7.58207D-03 |proj g|= 8.42580D-05 * * * 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 8.426D-05 7.582D-03 F = 7.5820667358142552E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.00019629] real 0m25.526s user 0m21.219s sys 0m0.678s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected) ================================================= xfoil: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/xfoil ================================================= + echo 'xfoil_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053] Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433] real 0m3.885s user 0m3.278s sys 0m0.136s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= awave: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/test/awave ================================================= + echo 'autoLink_Pytest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + python -u autoLink_Pytest.py -outLevel=0 -noPlotData + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/DARWIN_ARM64/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 = [[0.019540190626717628, 0.017418911634887138, 0.016377545441632904, 0.01572340736890536, 0.01529976634126216, 0.015051258605800992, 0.014977771651944392], [0.02003019062671763, 0.01782891163488714, 0.016737545441632903, 0.01606340736890536, 0.015619766341262161, 0.015351258605800992, 0.015267771651944394], [0.020570190626717628, 0.018268911634887138, 0.017127545441632905, 0.01642340736890536, 0.01594976634126216, 0.015671258605800993, 0.015577771651944392], [0.02114019062671763, 0.018738911634887136, 0.017547545441632905, 0.016813407368905357, 0.01631976634126216, 0.016011258605800993, 0.015907771651944392], [0.021770190626717627, 0.019248911634887136, 0.018007545441632904, 0.017233407368905357, 0.01671976634126216, 0.01639125860580099, 0.01626777165194439], [0.02246019062671763, 0.019808911634887138, 0.018507545441632904, 0.01769340736890536, 0.01713976634126216, 0.016801258605800992, 0.016657771651944393], [0.023210190626717628, 0.020418911634887137, 0.019047545441632903, 0.01819340736890536, 0.01760976634126216, 0.01724125860580099, 0.017077771651944393], [0.02425019062671763, 0.021258911634887138, 0.019797545441632904, 0.01887340736890536, 0.01824976634126216, 0.017851258605800994, 0.017657771651944393], [0.025430190626717628, 0.022218911634887137, 0.020637545441632904, 0.01965340736890536, 0.01897976634126216, 0.01853125860580099, 0.01830777165194439], [0.026710190626717627, 0.023248911634887136, 0.021547545441632905, 0.02048340736890536, 0.01975976634126216, 0.019271258605800992, 0.019007771651944394], [0.02810019062671763, 0.024358911634887136, 0.022527545441632903, 0.021383407368905358, 0.02058976634126216, 0.02006125860580099, 0.019757771651944395], [0.029590190626717628, 0.025548911634887136, 0.023577545441632902, 0.02233340736890536, 0.02148976634126216, 0.02090125860580099, 0.020557771651944393]] real 0m54.192s user 0m34.662s sys 0m8.770s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* All tests pass! ================================================= ================================================= ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest ++ ./execute_PyTestRegression.sh LINEARAERO ================================================= Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... LINEARAERO PyTests ================================================= + rm -rf avl_PyTest + echo 'avl_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 0.0006119078685800925 CYtot -6.292592518559147e-15 CZtot -0.3012861394881712 Cltot -4.783069014642483e-14 Cmtot -0.1945055953448147 Cntot -2.338890054396671e-15 Cl'tot -4.786422456048383e-14 Cn'tot -1.50377318550154e-15 CLtot 0.3012509314146395 CDtot 0.00464635348821979 CDvis 0.0 CLff 0.3009503023516151 CYff -7.7198870803959e-15 CDind 0.00464635348821979 CDff 0.004968969500894849 e 0.9669902146155998 StripForces Wing cl = [0.02994790451338, 0.08555545178909, 0.1329003532584, 0.1733025192691, 0.2100182422829, 0.2453427152542, 0.279274699636, 0.3101221284185, 0.3355632628219, 0.3531618776071, 0.3603457261529, 0.3542128805661, 0.3542128805657, 0.3603457261529, 0.3531618776083, 0.3355632628247, 0.3101221284231, 0.2792746996423, 0.2453427152618, 0.2100182422917, 0.1733025192796, 0.132900353272, 0.08555545180763, 0.0299479045407] Wing cd = [-0.004234137763148, -0.004494543653181, -0.003752887372721, -0.002739626801633, -0.001762021024329, -0.0007386538946456, 0.0005114598078319, 0.00211914728609, 0.00414518990896, 0.006609094404164, 0.009540018987574, 0.01315518814705, 0.01315518814715, 0.00954001898777, 0.006609094404422, 0.004145189909247, 0.002119147286374, 0.0005114598080921, -0.0007386538944123, -0.001762021024098, -0.002739626801367, -0.003752887372442, -0.004494543653152, -0.00423413776453] 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.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.001s user 0m0.647s sys 0m0.277s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Loading AIM ERROR:: (name_not_found) in Branch Brch_000083 at [[/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 -0.03128890430601078 CYtot 1.620300855394499e-10 CZtot -1.01466318148157 Cltot 8.675094643663818e-10 Cmtot -2.941985194288111 Cntot -1.437605900161857e-10 Cl'tot 8.648683702264562e-10 Cn'tot -1.588788223423184e-10 CLtot 1.013962576689473 CDtot 0.04899245309449728 CDvis 0.0 CLff 1.012753631213263 CYff 1.896406785878674e-10 CDind 0.04899245309449728 CDff -0.08941727830736593 e -0.6085342321688461 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: '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 0m10.295s user 0m9.314s sys 0m4.548s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 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 = 0.002572533601550775 Cl = 0.2009337808873524 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 = 0.002586364230241802 Cl = 0.2015191856814851 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 = 0.002609799718816161 Cl = 0.202507529643332 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 = 0.002643444008424624 Cl = 0.2039185811658769 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 = 0.002688200920998204 Cl = 0.2057816377790584 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 = 0.002745342060015943 Cl = 0.2081373840559949 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 = 0.002816610334298771 Cl = 0.2110406736705562 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 = 0.002904376657734716 Cl = 0.2145646488015997 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 = 0.003011879793042747 Cl = 0.2188068842334945 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 = 0.003143602034586226 Cl = 0.2238987294815726 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 = 0.003305877285452361 Cl = 0.2300199286487156 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 = 0.003507917885472537 Cl = 0.2374223860296633 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 = 0.003763643677259966 Cl = 0.2464707142744908 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 = 0.004095167898227208 Cl = 0.25771580677477 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 = 0.004540047408135333 Cl = 0.2720394012163583 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 = 0.005168237926851883 Cl = 0.2909701507463254 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 = 0.006128930715329168 Cl = 0.317487548593558 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 = 0.007818359051271666 Cl = 0.3586078919918751 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 = 0.01186220444373961 Cl = 0.4382638635243895 Cl[0] = 0.2009337808873524 Cd[0] = 0.002572533601550775 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.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m36.011s user 0m12.901s sys 0m13.126s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 -0.01911479917641001 CYtot 0.03828770401115553 CZtot -0.6203123021537938 Cltot 0.05803020542928473 Cmtot -0.3649415791575079 Cntot -0.02051317548232544 Cl'tot 0.05766336287208538 Cn'tot -0.02152281795713262 CLtot 0.6198842263414319 CDtot 0.02993783031514586 CDvis 0.0 CLff 0.6192452092592853 CYff 0.03287079625844261 CDind 0.02993783031514586 CDff 0.0286101982265777 e 0.7130586920543264 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.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.084s user 0m0.806s sys 0m0.322s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.867s user 0m0.736s sys 0m0.289s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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 = [1.13333237, 0.216380283] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.587s user 0m0.762s sys 0m0.126s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Loading AIM Setting Mach & Altitude Values Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Total drag = [0.0132, 0.01226] Form drag = [0.0033, 0.00307] Friction drag = [0.0099, 0.00919] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.585s user 0m0.607s sys 0m0.123s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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. Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG Getting results Cl = 0.933407 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 0m0.540s user 0m0.630s sys 0m0.113s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running xFoil...... Cl = [1.05475230551148, 1.36488869373725, 1.56607214272246, 2.03059709357768, 1.9727108312095, 1.87307153172323, 1.76050475760053] Cd = [0.0131991208831308, 0.0166540240605859, 0.0200551482562657, 0.0458671341873005, 0.0754256009397268, 0.0994469174479059, 0.127479430989221] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.49604411072842, 0.461377732041756, 0.442376568202227, 0.361251636144409, 0.276104140854608, 0.214381239321802, 0.132988264746433] 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 0m3.247s user 0m3.095s sys 0m0.142s + 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt + python -u autoLink_Pytest.py -verbosity=0 -workDir=runDirectory -noPlotData 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 = [[0.019540190626717628, 0.017418911634887138, 0.016377545441632904, 0.01572340736890536, 0.01529976634126216, 0.015051258605800992, 0.014977771651944392], [0.02003019062671763, 0.01782891163488714, 0.016737545441632903, 0.01606340736890536, 0.015619766341262161, 0.015351258605800992, 0.015267771651944394], [0.020570190626717628, 0.018268911634887138, 0.017127545441632905, 0.01642340736890536, 0.01594976634126216, 0.015671258605800993, 0.015577771651944392], [0.02114019062671763, 0.018738911634887136, 0.017547545441632905, 0.016813407368905357, 0.01631976634126216, 0.016011258605800993, 0.015907771651944392], [0.021770190626717627, 0.019248911634887136, 0.018007545441632904, 0.017233407368905357, 0.01671976634126216, 0.01639125860580099, 0.01626777165194439], [0.02246019062671763, 0.019808911634887138, 0.018507545441632904, 0.01769340736890536, 0.01713976634126216, 0.016801258605800992, 0.016657771651944393], [0.023210190626717628, 0.020418911634887137, 0.019047545441632903, 0.01819340736890536, 0.01760976634126216, 0.01724125860580099, 0.017077771651944393], [0.02425019062671763, 0.021258911634887138, 0.019797545441632904, 0.01887340736890536, 0.01824976634126216, 0.017851258605800994, 0.017657771651944393], [0.025430190626717628, 0.022218911634887137, 0.020637545441632904, 0.01965340736890536, 0.01897976634126216, 0.01853125860580099, 0.01830777165194439], [0.026710190626717627, 0.023248911634887136, 0.021547545441632905, 0.02048340736890536, 0.01975976634126216, 0.019271258605800992, 0.019007771651944394], [0.02810019062671763, 0.024358911634887136, 0.022527545441632903, 0.021383407368905358, 0.02058976634126216, 0.02006125860580099, 0.019757771651944395], [0.029590190626717628, 0.025548911634887136, 0.023577545441632902, 0.02233340736890536, 0.02148976634126216, 0.02090125860580099, 0.020557771651944393]] 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 1m0.905s user 0m35.963s sys 0m12.958s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* All tests pass! ================================================= ================================================= [Execution node] check if [viggen] 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/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [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/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [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/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [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/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [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/7.8/CAPS/LINEARAERO/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.8,ESPTEST=CAPS/LINEARAERO,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #632'. [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