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Started by upstream project "ESP_RegCaps" build number 619 originally caused by: Started by an SCM change Running as SYSTEM [EnvInject] - Loading node environment variables. Building remotely on windows10x64 in workspace C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019 [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Done Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\pyEGADS\pyEGADS\__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/EGADS at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ U trunk\src\egadsGeom.cpp At revision 2021 Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\custom\NMakefile Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\regressionTest\pyCAPSlog.txt Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\pyCAPS\autoLink_Pytest 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Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/CAPS at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A training\lectures Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A training\lectures\session02.tex A training\lectures\CAPSoptions.tex A training\lectures\session08.tex A training\lectures\Makefile A training\lectures\muddy_06_07.tex A training\lectures\muddy_08_09.tex A training\lectures\session09.tex A training\lectures\session11.tex A training\lectures\MUDDYoptions.tex A training\lectures\muddy_01_02.tex A training\lectures\muddy_03_04_05.tex A 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AU training\lectures\welcome\NASA.png A training\lectures\session04 A training\lectures\session04\save.view AU training\lectures\session04\wing4.png AU training\lectures\session04\wing4_CFDvisc.png AU training\lectures\session04\wing4_VLM.png AU training\lectures\session04\wing4_coupled.png AU training\lectures\session04\wing4_struct.png AU training\lectures\session04\transport.png AU training\lectures\session04\wing1.png A training\lectures\csmListing.tex A training\lectures\csmListingsBW.tex A training\lectures\session01 AU training\lectures\session01\ParaView_Logo.png AU training\lectures\session01\AIMdoc.png AU training\lectures\session01\inviscidTransport_Full.png A training\lectures\session08 A training\lectures\session08\logoSU2_v3_3_mod.png AU training\lectures\session08\hi_lift2.jpg AU training\lectures\session08\hl_crm_01.png AU training\lectures\session08\fun3d_logo.png AU training\lectures\session08\nasa_meatball_0138.png AU training\lectures\cmpress A training\lectures\PythonTutorial.tex A training\lectures\session02 AU training\lectures\session02\f118_boxter.png A training\lectures\session03 AU training\lectures\session03\avl_logo.png AU training\lectures\session03\naca.png AU training\lectures\session03\planevanilla.png AU training\lectures\session03\xfoil_logo.png A training\lectures\capsSyllabus.tex A training\lectures\oneTrainingSyllabus.tex AU training\lectures\questionnaire.docx A training\lectures\syllabus.tex A training\lectures\cover.tex A training\lectures\overlayPageSubNumber.tex A training\lectures\ParaviewBasics AU training\lectures\ParaviewBasics\basic_paraview.pdf AU training\lectures\ParaviewBasics\basic_paraview.pptx AU training\lectures\ParaviewBasics\Screen Shot 2019-04-26 at 12.41.32 PM.png AU training\lectures\ParaviewBasics\Screen Shot 2019-04-26 at 12.42.43 PM.png AU training\lectures\ParaviewBasics\Screen Shot 2019-04-26 at 12.43.22 PM.png AU training\lectures\ParaviewBasics\Screen Shot 2019-04-26 at 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C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP Updating svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A data\CAPS\csmOCCFailure_7.8.txt A data\TRADES\csmOCCFailure_7.8.txt A data\basic\csmOCCFailure_7.8.txt A data\capsExamples\csmOCCFailure_7.8.txt A data\csmIgnore_7.8.txt A data\csmOCCFailure_7.8.txt A data\gallery\csmOCCFailure_7.8.txt A data\legacy\csmOCCFailure_7.8.txt A data\studentGallery\csmOCCFailure_7.8.txt A data\training\csmOCCFailure_7.8.txt A data\vsp3\csmOCCFailure_7.8.txt A valgrind\valgrind-OCC7.8.supp At revision 849 Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src\epsilonpsi.mod Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src\naca456_main.mod Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src\naca456udpdata.mod Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src\nacaauxilary.mod Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\src\splineprocedures.mod Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2472 Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2472 Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\data Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A Slugs AU Slugs\damaged_1.stl A Slugs\verify_7.7.0 A Slugs\verify_7.7.0\blend12_1.vfy A Slugs\verify_7.7.0\blindeye_1.vfy A Slugs\verify_7.7.0\boxBall_1.vfy A Slugs\verify_7.7.0\boxHole_1.vfy A Slugs\verify_7.7.0\box_1.vfy A Slugs\verify_7.7.0\cylinderHole_1.vfy A Slugs\verify_7.7.0\cylinder_1.vfy A Slugs\verify_7.7.0\damaged_2.vfy A Slugs\verify_7.7.0\demo1_1.vfy A Slugs\verify_7.7.0\duct_1.vfy A Slugs\verify_7.7.0\eyeball_1.vfy A Slugs\verify_7.7.0\holes_1.vfy A Slugs\verify_7.7.0\pieslice_1.vfy A Slugs\verify_7.7.0\sphere_1.vfy A Slugs\verify_7.7.0\torus_1.vfy A Slugs\verify_7.7.0\tutorial1.vfy A Slugs\verify_7.7.0\wing_1.vfy A Slugs\verify_7.6.0 A Slugs\verify_7.6.0\blend12_1.vfy A Slugs\verify_7.6.0\blindeye_1.vfy A Slugs\verify_7.6.0\boxBall_1.vfy A Slugs\verify_7.6.0\boxHole_1.vfy A Slugs\verify_7.6.0\box_1.vfy A Slugs\verify_7.6.0\cylinderHole_1.vfy A Slugs\verify_7.6.0\cylinder_1.vfy A Slugs\verify_7.6.0\damaged_2.vfy A Slugs\verify_7.6.0\demo1_1.vfy A Slugs\verify_7.6.0\duct_1.vfy A Slugs\verify_7.6.0\eyeball_1.vfy A Slugs\verify_7.6.0\holes_1.vfy A Slugs\verify_7.6.0\pieslice_1.vfy A Slugs\verify_7.6.0\sphere_1.vfy A Slugs\verify_7.6.0\torus_1.vfy A Slugs\verify_7.6.0\tutorial1.vfy A Slugs\verify_7.6.0\wing_1.vfy A Slugs\holes_0.stl Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ A Slugs\boxBall_0.jrnl A Slugs\boxBall.plot A Slugs\boxBall_0.stl A Slugs\holes.plot A Slugs\holes_0.csm A Slugs\holes_0.jrnl A Slugs\holes_1.csm AU Slugs\tutorial1.stl A Slugs\sphere_0.stl A Slugs\blend12.plot A Slugs\blend12_0.csm A Slugs\blend12_0.stl A Slugs\blindeye.plot A Slugs\blindeye_0.csm A Slugs\blindeye_0.jrnl A Slugs\blindeye_0.stl A Slugs\blindeye_1.csm A Slugs\box.plot A Slugs\boxBall_0.csm A Slugs\boxBall_1.csm A Slugs\boxHole.plot A Slugs\boxHole_0.csm A Slugs\boxHole_0.jrnl A Slugs\boxHole_0.stl A Slugs\box_0.csm A Slugs\box_0.jrnl A Slugs\box_0.stl A Slugs\cylinder.plot A Slugs\cylinderHole.plot A Slugs\cylinderHole_0.csm A Slugs\cylinderHole_0.jrnl A Slugs\cylinderHole_0.stl A Slugs\cylinder_0.csm A Slugs\cylinder_0.jrnl A Slugs\cylinder_0.stl A Slugs\damaged.plot A Slugs\damaged_0.csm A Slugs\damaged_0.stl A Slugs\damaged_1.jrnl A Slugs\demo1.plot A Slugs\demo1_0.csm A Slugs\demo1_0.jrnl A Slugs\demo1_0.stl A Slugs\duct.plot A Slugs\duct_0.csm A Slugs\duct_0.jrnl A Slugs\duct_0.stl A Slugs\eyeball.plot A Slugs\eyeball_0.csm A Slugs\eyeball_0.jrnl A Slugs\eyeball_0.stl A Slugs\myGlider.plot A Slugs\myGlider_0.cpc A Slugs\myGlider_0.stl A Slugs\pieslice.plot A Slugs\pieslice_0.csm A Slugs\pieslice_0.jrnl A Slugs\pieslice_0.stl A Slugs\sphere.plot A Slugs\sphere_0.csm A Slugs\sphere_0.jrnl A Slugs\torus.plot A Slugs\torus_0.csm A Slugs\torus_0.jrnl A Slugs\torus_0.stl A Slugs\tutorial1.jrnl A Slugs\tutorial1.plot A Slugs\tutorial1_setup.csm A Slugs\tutorial1_setup.stl A Slugs\wing.plot A Slugs\wingBody.plot A Slugs\wingBody_0.cpc A Slugs\wingBody_0.stl A Slugs\wing_0.csm A Slugs\wing_0.jrnl A Slugs\wing_0.stl A Slugs\blend12_1.csm A Slugs\boxHole_1.csm A Slugs\box_1.csm A Slugs\cylinderHole_1.csm A Slugs\cylinder_1.csm A Slugs\damaged_2.csm A Slugs\demo1_1.csm A Slugs\duct_1.csm A Slugs\myGlider_2.csm A Slugs\sphere_1.csm A Slugs\torus_1.csm A Slugs\tutorial1.csm A Slugs\wingBody_2.csm A Slugs\wing_1.csm A Slugs\testfiles A Slugs\testfiles\elbow.stl A Slugs\testfiles\elbow_NW.csm A Slugs\testfiles\elbow_NW.jrnl A Slugs\testfiles\elbow_NW.stl A Slugs\testfiles\nucleus1.csm A Slugs\testfiles\nucleus1.jrnl A Slugs\testfiles\nucleus1.stl A Slugs\testfiles\nucleus2.stl A Slugs\testfiles\nucleus3.stl AU Slugs\aneurysm_case1.iges AU Slugs\aneurysm_case1_slugs.stl A Slugs\eyeball_1.csm A Slugs\pieslice_1.csm A Slugs\myGlider_0.jrnl A Slugs\myGlider_1.jrnl A Slugs\damaged_0.jrnl A Slugs\wingBody_0.jrnl A Slugs\wingBody_1.jrnl A Slugs\tutorial1_setup.jrnl A Slugs\blend12_0.jrnl At revision 2472 Cleaning up C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\pyOCSM Deleting C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\pyOCSM\pyOCSM\__pycache__ Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-03-05T22:19:11.419 -0500' Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ At revision 2472 Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ No changes for svn+ssh://acdl.mit.edu/home/svnroot/CAPS since the previous build Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’ No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/src since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/udc since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/data since the previous build No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM since the previous build [GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [Execution node] check if [windows10x64] is in [[macys, macys_VM, reynolds, viggen]] Run condition [Execution node ] preventing perform for step [Execute shell] [Execution node] check if [windows10x64] is in [[windows10x64]] Run condition [Execution node ] enabling perform for step [Execute Windows batch command] [WIN64.2019] $ cmd /c call C:\Users\jenkins\AppData\Local\Temp\jenkins3978696425570474946.bat C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>rmdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\training\lectures /S /Q C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if NOT CAPS/LINEARAERO == OpenCSM/data/Slugs (rmdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\data\Slugs /S /Q ) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Run the regression tests C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESP_Regression.bat C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM set PATH=C:\MinGW\msys\1.0\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PATH=C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM echo set WORKSPACE_BASH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>workspace.bat || exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep 5 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM bash.exe -c "sed -i 's/\\\/\//g' workspace.bat" || exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep 5 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM bash.exe -c "sed -i 's/C:/\/c/g' workspace.bat" || exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep 5 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM bash.exe -c "sed -i 's/D:/\/d/g' workspace.bat" || exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep 5 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM bash.exe -c "sed -i 's/[ \t]*$//' workspace.bat" || exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep 5 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM call workspace.bat C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Setup the environment C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESP_Env.bat C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set AFLR_VERSION=11.5.9 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set AFLR_ARCH=WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set VSP_VERSION=3.34.0 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHON_VERSION=3.11.6 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHON_MINOR=11 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Indicate that AWAVE should be compiled C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set AWAVE=awavemod.f C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set EMPnumProc=2 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM minimal output from CAPS by default C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set CAPS_OUTLEVEL=0 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM -------------- C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Windows 7 Env C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 ( if WIN64.2019 == WIN64.2010 call "D:\Compilers\Microsoft Visual Studio 10.0\VC\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2012 call "D:\Compilers\Microsoft Visual Studio 11.0\VC\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2013 call "D:\Compilers\Microsoft Visual Studio 12.0\VC\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2015 call "D:\Compilers\Microsoft Visual Studio 14.0\VC\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2017 call "D:\Compilers\Microsoft Visual Studio\2017\Community\VC\Auxiliary\Build\vcvarsall.bat" x64 echo on set PYTHONINC=D:\Anaconda2\include set PYTHONLIB=D:\Anaconda2\libs\python27.lib set CASROOT=D:\OpenCASCADE-7.6.1 set ESP_EXTERN_LIBS=D:\ESP_ExternLibs ) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM AFLR C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set AFLR=D:\AFLR\aflr_lib_11.5.9 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM astros C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set ASTROS_ROOT=D:\astros C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set PATH=;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM avl C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set PATH=D:\avl;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM delaundo C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set PATH=D:\delaundo;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM IRIT C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set IRIT_LIB=D:\IRIT\irit-win\lib64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set IRIT_INC=D:\IRIT\irit-sm C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set PATH=D:\IRIT\irit-win\ntbin64;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM mystran C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set MYSTRAN_directory=D:\mystran\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set PATH=;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM SU2 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set SU2_RUN=D:\SU2\SU2_Falcon\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set SU2_HOME=D:\SU2\SU2_Falcon C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set PATH=;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set PYTHONPATH=; C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM tetgen C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set TETGEN=D:\tetgen\tetgen1.6.0 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM tsfoil C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows7x64 set PATH=D:\tsfoil;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM xfoil C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows7x64 set PATH=D:\xfoil;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Windows 7 Env END C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM -------------- C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM -------------- C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Windows 10 Env C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 ( if WIN64.2019 == WIN64.2017 call "C:\Program Files (x86)\Microsoft Visual Studio\2017\Community\VC\Auxiliary\Build\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2019 call "C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Auxiliary\Build\vcvarsall.bat" x64 if WIN64.2019 == WIN64.2022 call "C:\Program Files\Microsoft Visual Studio\2022\Community\VC\Auxiliary\Build\vcvarsall.bat" x64 echo on set PYTHONINC=C:\Users\jenkins\ESP_Python-3.11.6\include set PYTHONLIB=C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib for / %D in ("C:\Users\jenkins\OpenCASCADE-7.6.*") do (set CASROOT=%D ) set ESP_EXTERN_LIBS=C:\Users\jenkins\ESP_ExternLibs ) ********************************************************************** ** Visual Studio 2019 Developer Command Prompt v16.11.32 ** Copyright (c) 2021 Microsoft Corporation ********************************************************************** [vcvarsall.bat] Environment initialized for: 'x64' C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>(set CASROOT=C:\Users\jenkins\OpenCASCADE-7.6.0 ) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM AFLR C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set AFLR=C:\Users\jenkins\AFLR\aflr_lib_11.5.9 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM astros C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows10x64 set ASTROS_ROOT=C:\Users\jenkins\astros C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows10x64 set PATH=;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM delaundo C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM IRIT C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set IRIT_LIB=C:\Users\jenkins\IRIT\irit-win\lib64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set IRIT_INC=C:\Users\jenkins\IRIT\irit-sm C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM OpenVSP C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set VSP3_ROOT=C:\Users\jenkins\OpenVSP\OpenVSP-3.34.0-win64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM tetgen C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set TETGEN=C:\Users\jenkins\tetgen\tetgen1.6.0 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM mystran C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set MYSTRAN_directory=C:\Users\jenkins\mystran\MYSTRAN_13.3A C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\mystran\MYSTRAN_13.3A;C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM SU2 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set SU2_HOME=C:\Users\jenkins\SU2\SU2-v7.1.1 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set SU2_RUN=C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\SU2\SU2-v7.1.1\bin;C:\Users\jenkins\mystran\MYSTRAN_13.3A;C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PYTHONPATH=;C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM tsfoil C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if windows10x64 == windows10x64 set PATH=C:\Users\jenkins\tsfoil;C:\Users\jenkins\SU2\SU2-v7.1.1\bin;C:\Users\jenkins\mystran\MYSTRAN_13.3A;C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM xfoil C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM if windows10x64==windows10x64 set PATH=C:\Users\jenkins\xfoil;C:\Users\jenkins\tsfoil;C:\Users\jenkins\SU2\SU2-v7.1.1\bin;C:\Users\jenkins\mystran\MYSTRAN_13.3A;C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Windows 10 Env END C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM -------------- C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM call "C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\em64t\bin\ifortvars.bat" C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call "C:\Program Files (x86)\Intel\oneAPI\setvars.bat" :: initializing oneAPI environment... Initializing Visual Studio command-line environment... Visual Studio version 16.11.32 environment configured. "C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\" Visual Studio command-line environment initialized for: 'x64' : compiler -- latest : debugger -- latest : dpl -- latest : mpi -- latest : tbb -- latest :: oneAPI environment initialized :: C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Reverse engineer ESP_ARCH and MSVC C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64.2019 == WIN64.2017 set MSVC=2017 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64.2019 == WIN64.2019 set MSVC=2019 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64.2019 == WIN64.2022 set MSVC=2022 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64.2019 == WIN64.2017 set ESP_ARCH=WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64.2019 == WIN64.2019 set ESP_ARCH=WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if WIN64 == WIN64.2022 set ESP_ARCH=WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if 7.6 == 7.3 if WIN64 == WIN64 set CASARCH=win64\vc14 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if 7.6 == 7.4 if WIN64 == WIN64 set CASARCH=win64\vc14 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if 7.6 == 7.6 if WIN64 == WIN64 set CASARCH=win64\vc14 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if 7.6 == 7.7 if WIN64 == WIN64 set CASARCH=win64\vc14 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set ESP_BLOC=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set ESP_ROOT=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM data for OpenCSM verification C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set CSMDATA=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\data C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PATH=C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\bin;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\env\..\redist\intel64\vc_mt;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\env\..\libfabric\bin\utils;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\env\..\libfabric\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\env\..\bin\release;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\env\..\bin;C:\Program Files (x86)\Intel\oneAPI\debugger\latest\env\\..\gdb\intel64\bin;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\bin;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\lib;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\bin\intel64;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\redist\intel64_win\compiler;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\lib\oclfpga\host\windows64\bin;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\lib\oclfpga\bin;C:\Users\jenkins\tsfoil;C:\Users\jenkins\SU2\SU2-v7.1.1\bin;C:\Users\jenkins\mystran\MYSTRAN_13.3A;C:\Users\jenkins\IRIT\irit-win\ntbin64;C:\Users\jenkins\delaundo;C:\Users\jenkins\ESP_Python-3.11.6\Scripts;C:\Users\jenkins\ESP_Python-3.11.6;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\\Extensions\Microsoft\IntelliCode\CLI;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Tools\MSVC\14.29.30133\bin\HostX64\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\VC\VCPackages;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TestWindow;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\CommonExtensions\Microsoft\TeamFoundation\Team Explorer;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\MSBuild\Current\bin\Roslyn;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Team Tools\Performance Tools;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\\x64;C:\Program Files (x86)\Microsoft Visual Studio\Shared\Common\VSPerfCollectionTools\vs2019\;C:\Program Files (x86)\Microsoft SDKs\Windows\v10.0A\bin\NETFX 4.8 Tools\x64\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\devinit;C:\Program Files (x86)\Windows Kits\10\bin\10.0.17763.0\x64;C:\Program Files (x86)\Windows Kits\10\bin\x64;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\\MSBuild\Current\Bin;C:\Windows\Microsoft.NET\Framework64\v4.0.30319;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\IDE\;C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\Common7\Tools\;C:\msys64\usr\bin;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\bin\release\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\;C:\Program Files (x86)\Intel\oneAPI\mpi\latest\libfabric\bin\utils\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\intel64\vc_mt\;C:\Program Files (x86)\Intel\oneAPI\tbb\latest\redist\ia32\vc_mt\;C:\Program Files\Common Files\Oracle\Java\javapath;C:\Program Files (x86)\Common Files\Oracle\Java\javapath;C:\ProgramData\Oracle\Java\javapath;C:\WINDOWS\system32;C:\WINDOWS;C:\WINDOWS\System32\Wbem;C:\WINDOWS\System32\WindowsPowerShell\v1.0\;C:\Program Files\Mosek\8\tools\platform\win64x86\bin;C:\WINDOWS\System32\OpenSSH\;C:\Program Files\TortoiseSVN\bin;C:\Program Files\Mosek\9.1\tools\platform\win64x86\bin;C:\Program Files\Git\cmd;C:\Anaconda2;C:\Anaconda2\Scripts;C:\Anaconda2\Library\bin;C:\Program Files (x86)\Intel\Compiler\Fortran\9.1\EM64T\Bin;C:\Program Files\Git\bin;C:\Users\jenkins\AppData\Local\Microsoft\WindowsApps;C:\Users\jenkins\AppData\Local\Programs\Python\Python38;C:\Users\jenkins\AppData\Local\Programs\Python\Python38\Scripts;%USERPROFILE%\AppData\Local\Microsoft\WindowsApps;C:\Program Files (x86)\Intel\oneAPI\compiler\latest\windows\lib\ocloc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM set PYTHONPATH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib;;C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHONPATH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\pyEGADS;;C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHONPATH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\pyOCSM;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\pyEGADS;;C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHONPATH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\pyOCSM;C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\pyEGADS;;C:\Users\jenkins\SU2\SU2-v7.1.1\bin C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM dissable python stdout buffering C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHONUNBUFFERED=true C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM https://docs.python.org/3/using/cmdline.html#envvar-PYTHONFAULTHANDLER C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set PYTHONFAULTHANDLER=true C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set UDUNITS2_XML_PATH=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\udunits\udunits2.xml C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>exit /b 0 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>if 0 NEQ 0 exit /b 666 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM ESP build from repository C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESPbfr.bat C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM Untar the build directories C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>"C:\Program Files\7-Zip\7z.exe" e C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESPbfr.tgz || exit /b 666 7-Zip [64] 15.14 : Copyright (c) 1999-2015 Igor Pavlov : 2015-12-31 Scanning the drive for archives: 1 file, 42058155 bytes (41 MiB) Extracting archive: C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESPbfr.tgz -- Path = C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\JenkinsESP\ESPbfr.tgz Type = gzip Headers Size = 10 Everything is Ok Size: 174295040 Compressed: 42058155 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>"C:\Program Files\7-Zip\7z.exe" x C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESPbfr.tar -x!*\DARWIN64\ || exit /b 666 7-Zip [64] 15.14 : Copyright (c) 1999-2015 Igor Pavlov : 2015-12-31 Scanning the drive for archives: 1 file, 174295040 bytes (167 MiB) Extracting archive: C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESPbfr.tar -- Path = C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESPbfr.tar Type = tar Physical Size = 174295040 Headers Size = 129024 Code Page = UTF-8 Everything is Ok Folders: 40 Files: 144 Size: 150070041 Compressed: 174295040 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM setup python virtualenv C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>virtualenv C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv || exit /b 666 created virtual environment CPython3.11.6.final.0-64 in 21203ms creator CPython3Windows(dest=C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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=C:\Users\jenkins\AppData\Local\pypa\virtualenv) added seed packages: pip==24.0, setuptools==69.0.3, wheel==0.42.0 activators BashActivator,BatchActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\activate.bat || exit /b 666 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>REM sleep random time so the install from multiple jobs is not simultaneous (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -c "import time; import random; time.sleep(random.randint(1,40))" (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>call :pip_install pip (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>set counter=0 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U pip Requirement already satisfied: pip in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (24.0) (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U 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 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U openmdao Collecting openmdao Using cached openmdao-3.30.0-py3-none-any.whl Collecting networkx>=2.0 (from openmdao) Using cached networkx-3.2.1-py3-none-any.whl.metadata (5.2 kB) Collecting numpy (from openmdao) Using cached numpy-1.26.4-cp311-cp311-win_amd64.whl.metadata (61 kB) Collecting scipy (from openmdao) Using cached scipy-1.12.0-cp311-cp311-win_amd64.whl.metadata (60 kB) Collecting requests (from openmdao) Using cached requests-2.31.0-py3-none-any.whl.metadata (4.6 kB) Collecting packaging (from openmdao) Using cached packaging-23.2-py3-none-any.whl.metadata (3.2 kB) Collecting charset-normalizer<4,>=2 (from requests->openmdao) Using cached charset_normalizer-3.3.2-cp311-cp311-win_amd64.whl.metadata (34 kB) Collecting idna<4,>=2.5 (from requests->openmdao) Using cached idna-3.6-py3-none-any.whl.metadata (9.9 kB) Collecting urllib3<3,>=1.21.1 (from requests->openmdao) Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB) Collecting certifi>=2017.4.17 (from requests->openmdao) Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB) Using cached networkx-3.2.1-py3-none-any.whl (1.6 MB) Using cached numpy-1.26.4-cp311-cp311-win_amd64.whl (15.8 MB) Using cached packaging-23.2-py3-none-any.whl (53 kB) Using cached requests-2.31.0-py3-none-any.whl (62 kB) Using cached scipy-1.12.0-cp311-cp311-win_amd64.whl (46.2 MB) Using cached certifi-2024.2.2-py3-none-any.whl (163 kB) Using cached charset_normalizer-3.3.2-cp311-cp311-win_amd64.whl (99 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, numpy, networkx, idna, charset-normalizer, certifi, scipy, requests, openmdao Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.6 networkx-3.2.1 numpy-1.26.4 openmdao-3.30.0 packaging-23.2 requests-2.31.0 scipy-1.12.0 urllib3-2.2.1 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U numpy Requirement already satisfied: numpy in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (1.26.4) (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U cvxopt Collecting cvxopt Using cached cvxopt-1.3.2-cp311-cp311-win_amd64.whl.metadata (1.4 kB) Using cached cvxopt-1.3.2-cp311-cp311-win_amd64.whl (12.8 MB) Installing collected packages: cvxopt Successfully installed cvxopt-1.3.2 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U 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 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U packaging Requirement already satisfied: packaging in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (23.2) (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U matplotlib Collecting matplotlib Using cached matplotlib-3.8.3-cp311-cp311-win_amd64.whl.metadata (5.9 kB) Collecting contourpy>=1.0.1 (from matplotlib) Using cached contourpy-1.2.0-cp311-cp311-win_amd64.whl.metadata (5.8 kB) Collecting cycler>=0.10 (from matplotlib) Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB) Collecting fonttools>=4.22.0 (from matplotlib) Using cached fonttools-4.49.0-cp311-cp311-win_amd64.whl.metadata (162 kB) Collecting kiwisolver>=1.3.1 (from matplotlib) Using cached kiwisolver-1.4.5-cp311-cp311-win_amd64.whl.metadata (6.5 kB) Requirement already satisfied: numpy<2,>=1.21 in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (from matplotlib) (1.26.4) Requirement already satisfied: packaging>=20.0 in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (from matplotlib) (23.2) Collecting pillow>=8 (from matplotlib) Using cached pillow-10.2.0-cp311-cp311-win_amd64.whl.metadata (9.9 kB) Collecting pyparsing>=2.3.1 (from matplotlib) Using cached pyparsing-3.1.1-py3-none-any.whl.metadata (5.1 kB) Collecting python-dateutil>=2.7 (from matplotlib) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB) Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib) Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB) Using cached matplotlib-3.8.3-cp311-cp311-win_amd64.whl (7.6 MB) Using cached contourpy-1.2.0-cp311-cp311-win_amd64.whl (187 kB) Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB) Using cached fonttools-4.49.0-cp311-cp311-win_amd64.whl (2.2 MB) Using cached kiwisolver-1.4.5-cp311-cp311-win_amd64.whl (56 kB) Using cached pillow-10.2.0-cp311-cp311-win_amd64.whl (2.6 MB) Using cached pyparsing-3.1.1-py3-none-any.whl (103 kB) Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB) Using cached six-1.16.0-py2.py3-none-any.whl (11 kB) Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib Successfully installed contourpy-1.2.0 cycler-0.12.1 fonttools-4.49.0 kiwisolver-1.4.5 matplotlib-3.8.3 pillow-10.2.0 pyparsing-3.1.1 python-dateutil-2.9.0.post0 six-1.16.0 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019>C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\venv\Scripts\python -m pip install --only-binary all -U scipy Requirement already satisfied: scipy in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (1.12.0) Requirement already satisfied: numpy<1.29.0,>=1.22.4 in c:\users\jenkins\workspace\esp_regcaps\7.6\caps\linearaero\win64.2019\esp\venv\lib\site-packages (from scipy) (1.26.4) 3 File(s) copied Compiling EGADS Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\*.c /Q /Y 24 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\*.cpp /Q /Y 9 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\*.h /Q /Y 7 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\*.rc /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\*.def /Q /Y 1 File(s) copied mkdir OCC cd OCC xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\OCC /S /Q /Y 14 File(s) copied cd .. mkdir Surreal cd Surreal xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\Surreal /S /Q /Y 7 File(s) copied cd .. xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\emp.c /Q /Y 1 File(s) copied copy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\evaluate.c evaluate.cpp /Y 1 file(s) copied. copy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\rational.c rational.cpp /Y 1 file(s) copied. xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\regQuads.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\regQuads.h /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\Surreal*_btest.cpp /Q /Y 4 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util\uvmap\uvmap_struct.h /Q /Y 1 File(s) copied del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\WIN64.2019 Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\WIN64.2019 copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\WIN64.2019 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\WIN64.2019 1 file(s) copied. cl /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE SurrealD1_btest.cpp /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD1.exe Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. SurrealD1_btest.cpp Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD1.exe SurrealD1_btest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD1 SurrealD1_test_suite Complete! cl /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE SurrealD4_btest.cpp /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD4.exe Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. SurrealD4_btest.cpp Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD4.exe SurrealD4_btest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealD4 SurrealD4_test_suite Complete! cl /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE SurrealS1_btest.cpp /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS1.exe Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. SurrealS1_btest.cpp Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS1.exe SurrealS1_btest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS1 SurrealS1_test_suite Complete! cl /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE SurrealS4_btest.cpp /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS4.exe Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. SurrealS4_btest.cpp Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS4.exe SurrealS4_btest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\SurrealS4 SurrealS4_test_suite Complete! cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\util nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap uvmap\main\uvmap.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmapFindUV.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmapFindUV.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmapGen.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmapGen.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmapStructFree.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmapStructFree.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_chk_edge_ratio.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_chk_edge_ratio.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmap_Read.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmap_Read.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmap_Write.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmap_Write.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\EG_uvmapTest.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_uvmapTest.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_test.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_test.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_add.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_add.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_bnd_adj.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_bnd_adj.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_chk_area_uv.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_chk_area_uv.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_cpu_message.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_cpu_message.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_find_uv.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_find_uv.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_from_egads.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_from_egads.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_gen.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_gen.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_gen_uv.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_gen_uv.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_ibeibe.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_ibeibe.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_ibfibf.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_ibfibf.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_ibfin.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_ibfin.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_iccibe.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_iccibe.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_iccin.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_iccin.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_idibe.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_idibe.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_inibe.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_inibe.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_inl_uv_bnd.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_inl_uv_bnd.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_malloc.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_malloc.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_mben_disc.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_mben_disc.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_message.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_message.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_norm_uv.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_norm_uv.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_read.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_read.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_solve.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_solve.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_struct_tasks.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_struct_tasks.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_to_egads.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_to_egads.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_version.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_version.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ uvmap\uvmap_write.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uvmap_write.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Iuvmap\. egadsUVmap.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egadsUVmap.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsUVmap.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\uvmap.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\uvmap.lib cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\uvmap.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egadsUVmap.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmapFindUV.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmapGen.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmapStructFree.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_chk_edge_ratio.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmap_Read.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmap_Write.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_uvmapTest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_test.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_add.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_bnd_adj.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_chk_area_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_cpu_message.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_find_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_from_egads.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_gen.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_gen_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_ibeibe.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_ibfibf.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_ibfin.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_iccibe.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_iccin.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_idibe.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_inibe.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_inl_uv_bnd.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_malloc.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_mben_disc.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_message.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_norm_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_read.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_solve.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_struct_tasks.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_to_egads.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap_write.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\util cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\uvmap.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib uvmap.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\uvmap.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib uvmap.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\uvmap.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\umap.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\umap.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\umap.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\umap.exe;1 cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsGeom.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsGeom.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsHLevel.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsHLevel.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsTopo.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTopo.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsCopy.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsCopy.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsIO.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsIO.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsSplineFit.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsSplineFit.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsSpline.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsSpline.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsTessSens.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTessSens.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include egadsSkinning.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsSkinning.cpp cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsBase.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsBase.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsMemory.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsMemory.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsAttrs.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsAttrs.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsTessInp.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTessInp.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsTess.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTess.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsTris.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTris.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsQuads.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsQuads.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsRobust.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsRobust.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsSBO.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsSBO.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsFit.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsFit.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap prmCfit.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. prmCfit.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap prmGrid.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. prmGrid.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap prmUV.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. prmUV.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsExport.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsExport.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsSolids.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsSolids.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I..\util /I..\util\uvmap egadsEffect.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsEffect.c cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include OCC\BRepLib_FuseEdges.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. BRepLib_FuseEdges.cpp cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include emp.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. emp.c cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IOCC /IC:\Users\jenkins\OpenCASCADE-7.6.0\inc /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I. evaluate.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. evaluate.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 rational.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. rational.cpp cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include /I. regQuads.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. regQuads.c rc egads Microsoft (R) Windows (R) Resource Compiler Version 10.0.10011.16384 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll /dll /def:egads.def egadsGeom.obj egadsHLevel.obj egadsTopo.obj egadsCopy.obj egadsIO.obj egadsSplineFit.obj egadsSpline.obj egadsTessSens.obj egadsSkinning.obj egadsBase.obj egadsMemory.obj egadsAttrs.obj egadsTessInp.obj egadsTess.obj egadsTris.obj egadsQuads.obj egadsRobust.obj egadsSBO.obj egadsFit.obj prmCfit.obj prmGrid.obj prmUV.obj egadsExport.obj egadsSolids.obj egadsEffect.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\BRepLib_FuseEdges.obj emp.obj evaluate.obj rational.obj regQuads.obj egads.res C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\uvmap.lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib TKBool.lib TKernel.lib TKFeat.lib TKBO.lib TKGeomAlgo.lib TKMath.lib TKOffset.lib TKPrim.lib TKTopAlgo.lib TKBRep.lib TKG2d.lib TKG3d.lib TKGeomBase.lib TKShHealing.lib TKSTEP.lib TKSTEP209.lib TKSTEPBase.lib TKSTEPAttr.lib TKXSBase.lib TKIGES.lib TKFillet.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.dll;2 del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadstatic.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadstatic.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadstatic.lib egadsBase.obj egadsMemory.obj egadsAttrs.obj egadsTessInp.obj egadsTess.obj egadsTris.obj egadsQuads.obj egadsRobust.obj egadsSBO.obj egadsFit.obj prmCfit.obj prmGrid.obj prmUV.obj egadsExport.obj egadsSolids.obj egadsEffect.obj egadsGeom.obj egadsHLevel.obj egadsTopo.obj egadsCopy.obj egadsIO.obj egadsSplineFit.obj egadsSpline.obj egadsTessSens.obj egadsSkinning.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\BRepLib_FuseEdges.obj emp.obj evaluate.obj rational.obj regQuads.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\uvmap.lib Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsBase.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsBase.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsMemory.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsMemory.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsAttrs.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsAttrs.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsTess.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsTess.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsGeom.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsGeom.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsHLevel.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsHLevel.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include fgadsTopo.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fgadsTopo.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fgads.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fgads.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fgads.lib fgadsBase.obj fgadsMemory.obj fgadsAttrs.obj fgadsTess.obj fgadsGeom.obj fgadsHLevel.obj fgadsTopo.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\emp.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\emp.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\emp.lib emp.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egads.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads_dot.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads_dot.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egads_dot.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads_dot.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.inc Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.inc copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egads.inc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egads.inc 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsErrors.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsErrors.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egadsErrors.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsErrors.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTypes.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTypes.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egadsTypes.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTypes.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\emp.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\emp.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\emp.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\emp.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\prm.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\prm.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\prm.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\prm.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\wsserver.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.inc Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.inc copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\wsserver.inc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsserver.inc 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsss.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsss.h copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\wsss.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\wsss.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTris.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTris.h copy /Y egadsTris.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsTris.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineFit.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineFit.h copy /Y egadsSplineFit.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineFit.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineVels.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineVels.h copy /Y egadsSplineVels.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsSplineVels.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsf90.inc Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsf90.inc copy /Y C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src\..\include\egadsf90.inc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egadsf90.inc 1 file(s) copied. copy /Y Surreal\SurrealD.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD.h 1 file(s) copied. copy /Y Surreal\SurrealD_Lazy.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Lazy.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Lazy.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Lazy.h 1 file(s) copied. copy /Y Surreal\SurrealD_Trad.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Trad.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Trad.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealD_Trad.h 1 file(s) copied. copy /Y Surreal\SurrealS.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS.h 1 file(s) copied. copy /Y Surreal\SurrealS_Lazy.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Lazy.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Lazy.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Lazy.h 1 file(s) copied. copy /Y Surreal\SurrealS_Trad.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Trad.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Trad.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\SurrealS_Trad.h 1 file(s) copied. copy /Y Surreal\always_inline.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\always_inline.h 1 file(s) copied. copy /B C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\always_inline.h+,, C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\Surreal\always_inline.h 1 file(s) copied. del *.cpp *.c *.h *.rc *def *.manifest del OCC\* /Q rmdir OCC del Surreal\* /Q rmdir Surreal cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\src Makefile NMakefile OCC Surreal egads.def egads.rc egadsAttrs.c egadsBase.c egadsClasses.h egadsCopy.cpp egadsEffect.c egadsExport.c egadsFit.c egadsGeom.cpp egadsHLevel.cpp egadsIO.cpp egadsInternals.h egadsMemory.c egadsOCC.h egadsQuads.c egadsRobust.c egadsSBO.c egadsSkinning.cpp egadsSolids.c egadsSpline.cpp egadsSplineFit.cpp egadsSplineFit.h egadsSplineVels.h egadsStack.h egadsTess.c egadsTessInp.c egadsTessSens.cpp egadsTopo.cpp egadsTris.c egadsTris.h elint fgadsAttrs.c fgadsBase.c fgadsGeom.c fgadsHLevel.c fgadsMemory.c fgadsTess.c fgadsTopo.c fgv.c flint make.bat prmCfit.c prmGrid.c prmUV.c EGADS Build Complete! Makefile NMakefile OCC Surreal egads.def egads.rc egadsAttrs.c egadsBase.c egadsClasses.h egadsCopy.cpp egadsEffect.c egadsExport.c egadsFit.c egadsGeom.cpp egadsHLevel.cpp egadsIO.cpp egadsInternals.h egadsMemory.c egadsOCC.h egadsQuads.c egadsRobust.c egadsSBO.c egadsSkinning.cpp egadsSolids.c egadsSpline.cpp egadsSplineFit.cpp egadsSplineFit.h egadsSplineVels.h egadsStack.h egadsTess.c egadsTessInp.c egadsTessSens.cpp egadsTopo.cpp egadsTris.c egadsTris.h elint fgadsAttrs.c fgadsBase.c fgadsGeom.c fgadsHLevel.c fgadsMemory.c fgadsTess.c fgadsTopo.c fgv.c flint make.bat prmCfit.c prmGrid.c prmUV.c Compiling EGADS wvServer Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\*.c /Q /Y 16 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\*.cpp /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\*.h /Q /Y 4 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\*.def /Q /Y 1 File(s) copied cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /DSTANDALONE /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers server.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\servertest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. server.c cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE map.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\map.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. map.cpp cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib gettimeofday.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. gettimeofday.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib websock-w32.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. websock-w32.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib base64-decode.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. base64-decode.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib handshake.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. handshake.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib client-handshake.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. client-handshake.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib libwebsockets.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. libwebsockets.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib extension-deflate-stream.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. extension-deflate-stream.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib md5.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. md5.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib extension-x-google-mux.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. extension-x-google-mux.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib parsers.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. parsers.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib extension.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. extension.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib sha-1.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. sha-1.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib browserMessage.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. browserMessage.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib server.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. server.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib wv.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. wv.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /D_UNICODE /DUNICODE /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\win32helpers fwv.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fwv.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fwv.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsservers.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsservers.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsservers.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\map.obj gettimeofday.obj websock-w32.obj base64-decode.obj handshake.obj client-handshake.obj libwebsockets.obj extension-deflate-stream.obj md5.obj extension-x-google-mux.obj parsers.obj extension.obj sha-1.obj browserMessage.obj server.obj wv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fwv.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib\*.c /Q /Y 15 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib\*.h /Q /Y 11 File(s) copied cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. adler32.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. adler32.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. gzclose.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. gzclose.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. gzwrite.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. gzwrite.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. inftrees.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. inftrees.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. compress.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. compress.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. infback.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. infback.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. trees.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. trees.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. crc32.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. crc32.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. gzlib.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. gzlib.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. inffast.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. inffast.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. uncompr.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. uncompr.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. deflate.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. deflate.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. gzread.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. gzread.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. inflate.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. inflate.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DNDEBUG /DWIN32 /D_CONSOLE /D_UNICODE /DUNICODE /I. zutil.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. zutil.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib adler32.obj gzclose.obj gzwrite.obj inftrees.obj compress.obj infback.obj trees.obj crc32.obj gzlib.obj inffast.obj uncompr.obj deflate.obj gzread.obj inflate.obj zutil.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del *.c *.h cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer\zlib cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\servertest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsservers.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib ws2_32.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\servertest.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsservers.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib ws2_32.lib echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\server.exe;1 del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.dll /dll /def:wsserver.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\map.obj gettimeofday.obj websock-w32.obj base64-decode.obj handshake.obj client-handshake.obj libwebsockets.obj extension-deflate-stream.obj md5.obj extension-x-google-mux.obj parsers.obj extension.obj sha-1.obj browserMessage.obj server.obj wv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\z.lib ws2_32.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.exp del *.c *.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\*.c cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\wvServer Compiling EGADS lite Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\*.c /Q /Y 23 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\*.h /Q /Y 6 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\*.rc /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\*.def /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\*.h /Q /Y 7 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsTess.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsTris.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsQuads.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsTessInp.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsRobust.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src\egadsEffect.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\emp.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\evaluate.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\rational.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\regQuads.c /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\regQuads.h /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\uvmap\uvmap_struct.h /Q /Y 1 File(s) copied cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteBase.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteBase.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteMemory.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteMemory.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteGeom.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteGeom.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteTopo.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteTopo.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteAttrs.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteAttrs.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteImport.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteImport.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /I..\util\uvmap liteString.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteString.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src egadsTess.c /FoliteTess.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTess.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src egadsTris.c /FoliteTris.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTris.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src egadsQuads.c /FoliteQuads.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsQuads.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src egadsTessInp.c /FoliteTessInp.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTessInp.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include evaluate.c /FoevaLite.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. evaluate.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE rational.c /ForatLite.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. rational.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /I. regQuads.c /FoliteRegQuads.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. regQuads.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src egadsEffect.c /FoliteEffect.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsEffect.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /DLITE /I. /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\src /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite\..\util\uvmap liteUVmap.c /FoliteUVmap.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. liteUVmap.c rc egadslite Microsoft (R) Windows (R) Resource Compiler Version 10.0.10011.16384 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll /dll /def:egadslite.def liteBase.obj liteMemory.obj liteGeom.obj liteTopo.obj liteAttrs.obj liteImport.obj liteString.obj liteTess.obj liteTris.obj liteQuads.obj liteTessInp.obj emp.obj evaLite.obj ratLite.obj egadsRobust.obj liteRegQuads.obj liteEffect.obj liteUVmap.obj egadslite.res Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslite.dll;2 del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslitestatic.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslitestatic.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadslitestatic.lib liteBase.obj liteMemory.obj liteGeom.obj liteTopo.obj liteAttrs.obj liteImport.obj liteString.obj liteTess.obj liteTris.obj liteQuads.obj liteTessInp.obj egadsRobust.obj emp.obj evaLite.obj ratLite.obj liteRegQuads.obj liteEffect.obj liteUVmap.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del *.c *.h *.rc *.def *.manifest cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\EGADS\trunk\lite Compiling OpenCSM Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers serveCSM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveCSM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. serveCSM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include OpenCSM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\OpenCSM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. OpenCSM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udp.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udp.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udp.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers tim.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tim.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. tim.c rc ocsm Microsoft (R) Windows (R) Resource Compiler Version 10.0.10011.16384 Copyright (C) Microsoft Corporation. All rights reserved. copy ocsm.res C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ocsm.res 1 file(s) copied. del ocsm.res del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll /dll /def:ocsm.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\OpenCSM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udp.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tim.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ocsm.res /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib wsserver.lib egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.dll;2 cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveCSM.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib wsserver.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib wsserver.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveCSM.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveCSM.exe;1 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers serveESP.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveESP.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. serveESP.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveESP.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib wsserver.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib wsserver.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\serveESP.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\serveESP.exe;1 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include sensCSM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\sensCSM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. sensCSM.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\sensCSM.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib ocsm.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\sensCSM.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\sensCSM.exe;1 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpBezier.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBezier.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpBezier.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBezier.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bezier.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpBiconvex.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBiconvex.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpBiconvex.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBiconvex.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\biconvex.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpBox.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBox.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpBox.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBox.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\box.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpBspline.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBspline.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpBspline.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpBspline.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\bspline.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfCatmull.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCatmull.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfCatmull.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCatmull.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\catmull.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfCompare.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCompare.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfCompare.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCompare.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\compare.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfCreateBEM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCreateBEM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfCreateBEM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCreateBEM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createBEM.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfCreatePoly.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCreatePoly.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfCreatePoly.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfCreatePoly.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\createPoly.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpCsm.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpCsm.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpCsm.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpCsm.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\csm.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfDeform.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDeform.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfDeform.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDeform.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\deform.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfDroop.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDroop.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfDroop.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDroop.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\droop.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfDumpPmtrs.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDumpPmtrs.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfDumpPmtrs.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfDumpPmtrs.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\dumpPmtrs.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfEditAttr.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfEditAttr.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfEditAttr.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfEditAttr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\editAttr.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpEllipse.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpEllipse.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpEllipse.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpEllipse.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ellipse.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpEqn2body.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpEqn2body.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpEqn2body.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpEqn2body.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\eqn2body.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpFitcurve.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpFitcurve.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpFitcurve.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpFitcurve.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fitcurve.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfFlend.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfFlend.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfFlend.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfFlend.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flend.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpFreeform.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpFreeform.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpFreeform.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpFreeform.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\freeform.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfGanged.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfGanged.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfGanged.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfGanged.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ganged.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfGuide.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfGuide.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfGuide.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfGuide.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\guide.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpHex.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpHex.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpHex.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpHex.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hex.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpImport.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpImport.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpImport.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpImport.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\import.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpKulfan.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpKulfan.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpKulfan.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpKulfan.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\kulfan.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfLinalg.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfLinalg.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfLinalg.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfLinalg.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\linalg.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfMatchBodys.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfMatchBodys.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfMatchBodys.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfMatchBodys.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\matchBodys.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfMechanism.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfMechanism.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfMechanism.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfMechanism.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mechanism.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpNaca.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNaca.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpNaca.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNaca.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfNaca6mc.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNaca6mc.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfNaca6mc.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNaca6mc.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca6mc.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfNacelle.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNacelle.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfNacelle.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNacelle.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nacelle.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpNurbbody.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNurbbody.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpNurbbody.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNurbbody.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nurbbody.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfNuscale.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNuscale.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfNuscale.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfNuscale.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nuscale.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfOffset.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfOffset.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfOffset.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfOffset.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\offset.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpParabaloid.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpParabaloid.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpParabaloid.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpParabaloid.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parabaloid.dll;2 cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpParsec.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpParsec.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpParsec.cpp del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpParsec.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\parsec.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpPod.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpPod.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpPod.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpPod.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pod.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpPoly.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpPoly.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpPoly.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpPoly.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\poly.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfPrintBbox.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintBbox.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfPrintBbox.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintBbox.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBbox.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfPrintBrep.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintBrep.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfPrintBrep.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintBrep.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printBrep.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfPrintEgo.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintEgo.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfPrintEgo.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfPrintEgo.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\printEgo.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpProp.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpProp.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpProp.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpProp.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\prop.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpRadwaf.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpRadwaf.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpRadwaf.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpRadwaf.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\radwaf.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpSample.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSample.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpSample.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSample.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sample.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpSew.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSew.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpSew.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSew.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\sew.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfShadow.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfShadow.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfShadow.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfShadow.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\shadow.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfSlices.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfSlices.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfSlices.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfSlices.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slices.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpStag.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpStag.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpStag.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpStag.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stag.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfStiffener.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfStiffener.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfStiffener.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfStiffener.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\stiffener.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpSupell.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSupell.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpSupell.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpSupell.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\supell.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udfTester1.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfTester1.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udfTester1.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udfTester1.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester1.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpTester2.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpTester2.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpTester2.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpTester2.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tester2.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpVsp3.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpVsp3.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpVsp3.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpVsp3.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vsp3.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpWaffle.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpWaffle.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpWaffle.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpWaffle.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\waffle.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpWarp.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpWarp.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpWarp.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpWarp.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\warp.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include eggPDT2.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\eggPDT2.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. eggPDT2.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll /dll /def:egg.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\eggPDT2.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\PDT2.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include udpNaca456.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNaca456.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. udpNaca456.c ifort /c /Ox /threads /recursive /libs:dll naca456.f90 /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\naca456.obj Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll /dll /def:udp.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\udpNaca456.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\naca456.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\naca456.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timEreped.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timEreped.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timEreped.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timEreped.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ereped.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timMitten.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timMitten.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timMitten.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timMitten.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mitten.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timPlotter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPlotter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timPlotter.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPlotter.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plotter.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timPlugs.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPlugs.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timPlugs.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPlugs.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\plugs.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timSlugs.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timSlugs.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timSlugs.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timSlugs.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\slugs.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timVspSetup.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timVspSetup.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timVspSetup.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timVspSetup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\vspSetup.dll;2 del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\OpenCSM.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\OpenCSM.h copy OpenCSM.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\OpenCSM.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\common.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\common.h copy common.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\common.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udp.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udp.h copy udp.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udp.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\esp.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\esp.h copy esp.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\esp.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\tim.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\tim.h copy tim.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\tim.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egg.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egg.h copy egg.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\egg.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.h copy udpUtilities.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.c Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.c copy udpUtilities.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\udpUtilities.c 1 file(s) copied. Compiling CAPS Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd src nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\caps.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\caps.h copy ..\include\caps.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\caps.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsErrors.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsErrors.h copy ..\include\capsErrors.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsErrors.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsTypes.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsTypes.h copy ..\include\capsTypes.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\capsTypes.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimUtil.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimUtil.h copy ..\include\aimUtil.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimUtil.h 1 file(s) copied. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimMesh.h Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimMesh.h copy ..\include\aimMesh.h C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aimMesh.h 1 file(s) copied. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\src\*.c /Q /Y 19 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\src\*.h /Q /Y 3 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\src\*.rc /Q /Y 1 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\src\*.def /Q /Y 3 File(s) copied cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsBase.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsBase.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsAnalysis.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsAnalysis.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsApprox.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsApprox.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsAttr.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsAttr.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsAIM.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsBound.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsBound.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsProblem.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsProblem.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsValue.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsValue.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsUnits.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsUnits.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsChkInpt.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsChkInpt.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include conjGrad.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. conjGrad.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include capsFunIDs.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. capsFunIDs.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include printObject.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. printObject.c rc caps Microsoft (R) Windows (R) Resource Compiler Version 10.0.10011.16384 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll /dll /def:caps.def capsBase.obj capsAnalysis.obj capsApprox.obj capsAttr.obj capsAIM.obj capsBound.obj capsProblem.obj capsValue.obj capsUnits.obj capsChkInpt.obj conjGrad.obj capsFunIDs.obj printObject.obj caps.res C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\udunits2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Advapi32.lib Ws2_32.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.dll;2 del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsstatic.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsstatic.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsstatic.lib capsBase.obj capsAnalysis.obj capsApprox.obj capsAttr.obj capsAIM.obj capsBound.obj capsProblem.obj capsValue.obj capsUnits.obj capsChkInpt.obj conjGrad.obj capsFunIDs.obj printObject.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include testingAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\testingAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. testingAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include aimUtil.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimUtil.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aimUtil.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include aimTransferUtil.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimTransferUtil.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aimTransferUtil.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include aimMesh.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimMesh.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aimMesh.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aimUtil.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aimUtil.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aimUtil.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimUtil.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimMesh.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimTransferUtil.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll /dll /def:aim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\testingAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib/aimUtil.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\udunits2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingAIM.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include testingWriter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\testingWriter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. testingWriter.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll /dll /def:testingWriter.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\testingWriter.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib/aimUtil.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\testingWriter.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include phaseUtil.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\phaseUtil.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. phaseUtil.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\phaseUtil.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\phaseUtil.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\phaseUtil.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\phaseUtil.obj del *.c *.h *.rc *.def cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\src cd ..\aim nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd utils nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /Icython /DHAVE_PYTHON /IC:\Users\jenkins\ESP_Python-3.11.6\include C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\attrUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\meshUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\cfdUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\miscUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\feaUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\vlmUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\nastranUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\tecplotUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\arrayUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\deprecateUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\cardUtils.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\nastranCards.c C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\jsonUtils.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. attrUtils.c meshUtils.c cfdUtils.c miscUtils.c feaUtils.c vlmUtils.c nastranUtils.c tecplotUtils.c arrayUtils.c deprecateUtils.c cardUtils.c nastranCards.c jsonUtils.c Generating Code... cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\vlmSpanSpace.cpp Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. vlmSpanSpace.cpp cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\ESP_Python-3.11.6\include C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\cython\nastranOP2Reader.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. nastranOP2Reader.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\utils.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\utils.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\utils.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\attrUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\meshUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cfdUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\miscUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\feaUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vlmUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\nastranUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tecplotUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\arrayUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\deprecateUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cardUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\nastranCards.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\jsonUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vlmSpanSpace.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\nastranOP2Reader.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aim\utils mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aim\utils cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\aim\utils xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\utils\*.h /Q /Y 21 File(s) copied cd .. cd avl nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils avlAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. avlAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ -Iavlmrf avlmrf\avlRead_BODY.c avlmrf\avlRead_CPOML.c avlmrf\avlRead_DERMATM.c avlmrf\avlRead_ELE.c avlmrf\avlRead_STRP.c avlmrf\avlRead_TOT.c avlmrf\avlRead_CNC.c avlmrf\avlRead_DERMATB.c avlmrf\avlRead_DERMATS.c avlmrf\avlRead_HINGE.c avlmrf\avlRead_SURF.c avlmrf\avlRead_VM.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. avlRead_BODY.c avlRead_CPOML.c avlRead_DERMATM.c avlRead_ELE.c avlRead_STRP.c avlRead_TOT.c avlRead_CNC.c avlRead_DERMATB.c avlRead_DERMATS.c avlRead_HINGE.c avlRead_SURF.c avlRead_VM.c Generating Code... del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll /dll /def:avlAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_BODY.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_CPOML.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_DERMATM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_ELE.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_STRP.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_TOT.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_CNC.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_DERMATB.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_DERMATS.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_HINGE.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_SURF.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlRead_VM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib utils.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\avlAIM.dll;2 cd .. cd cbaero nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I..\meshWriter\fastWriter cbaeroAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cbaeroAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. cbaeroAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll /dll /def:cbaeroAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cbaeroAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\cbaeroAIM.dll;2 cd .. cd delaundo nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils delaundoAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\delaundoAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. delaundoAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll /dll /def:delaundoAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\delaundoAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\delaundoAIM.dll;2 cd .. cd egadsTess nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils egadsTessAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egadsTessAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. egadsTessAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll /dll /def:egadsTessAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egadsTessAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egadsTessAIM.dll;2 cd .. cd friction nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils frictionAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\frictionAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. frictionAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll /dll /def:frictionAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\frictionAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\frictionAIM.dll;2 ifort /c /Ox /threads /recursive /libs:dll friction_eja_mod.f /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\friction.obj Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\friction.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\friction.obj Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. -out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\friction.exe -subsystem:console C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\friction.obj cd .. cd fun3d nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I..\meshWriter\ugridWriter /IC:\Users\jenkins\ESP_Python-3.11.6\include /Icython /DHAVE_PYTHON fun3dAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fun3dAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I..\meshWriter\ugridWriter /I. fun3dUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fun3dUtils.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /IC:\Users\jenkins\ESP_Python-3.11.6\include cython/fun3dNamelist.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dNamelist.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fun3dNamelist.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll /dll /def:fun3dAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dNamelist.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fun3dAIM.dll;2 cd .. cd abaqus nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I. abaqusAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. abaqusAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I. /IC:\Users\jenkins\ESP_Python-3.11.6\include /Icython /DHAVE_PYTHON abaqusUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. abaqusUtils.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils /I. /IC:\Users\jenkins\ESP_Python-3.11.6\include cython\abaqusFILReader.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusFILReader.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. abaqusFILReader.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll /dll /def:abaqusAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\abaqusFILReader.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\abaqusAIM.dll;2 cd .. cd mystran nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils mystranAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. mystranAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils mystranUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. mystranUtils.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll /dll /def:mystranAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranUtils.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\mystranAIM.dll;2 cd .. cd masstran nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils masstranAIM.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\masstranAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. masstranAIM.cpp del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll /dll /def:masstranAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\masstranAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\masstranAIM.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 Masstran.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Masstran.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Masstran.c cl C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Masstran.obj /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\Masstran.exe Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\Masstran.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Masstran.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\Masstran.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\Masstran.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\Masstran.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\Masstran.exe;1 cd .. cd nastran nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils nastranAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\nastranAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. nastranAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll /dll /def:nastranAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\nastranAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\nastranAIM.dll;2 cd .. cd meshWriter nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. forfiles /m *Writer /c "cmd /c if @isdir==TRUE echo Build @file & cd @file & nmake -f NMakefile" Build "exodusWriter" Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Build "fastWriter" Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include fastWriter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fastWriter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fastWriter.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll /dll /def:fastWriter.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fastWriter.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\fastWriter.dll;2 Build "libMeshbWriter" Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include libMeshbWriter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\libMeshbWriter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. libMeshbWriter.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IlibMeshb\sources libMeshb\sources\libmeshb7.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\libmeshb7.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. libmeshb7.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll /dll /def:libMeshbWriter.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\libMeshbWriter.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\libmeshb7.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\libMeshbWriter.dll;2 Build "su2Writer" Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include su2Writer.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2Writer.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2Writer.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll /dll /def:su2Writer.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2Writer.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2Writer.dll;2 Build "ugridWriter" Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include ugridWriter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ugridWriter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. ugridWriter.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll /dll /def:ugridWriter.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\ugridWriter.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ugridWriter.dll;2 cd .. cd pointwise nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils pointwiseAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\pointwiseAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. pointwiseAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils hashElement.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hashElement.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hashElement.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll /dll /def:pointwiseAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\pointwiseAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hashElement.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pointwiseAIM.dll;2 cd .. cd astros nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils astrosAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. astrosAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils astrosUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. astrosUtils.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils astrosCards.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosCards.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. astrosCards.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll /dll /def:astrosAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\astrosCards.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\astrosAIM.dll;2 cd .. cd hsm nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils hsmAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils hsmUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj/hsmUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmUtils.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils hsmAdj.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj/hsmAdj.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmAdj.c cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 rcm\rcm.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\rcm.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. rcm.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 rcm\genrcmi.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj/genrcmi.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. genrcmi.cpp cd src nmake -f nmakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\hsm\src\*.f /Q /Y 19 File(s) copied xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\hsm\src\*.inc /Q /Y 4 File(s) copied ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmsol.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmdep.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmout.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmgeo.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmabd.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmeqn.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmbc.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmprj.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmren.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmre1.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmrfm.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmbb2.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. hsmglr.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. ludcmp.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. sbsolve.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. atanc.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. bmdump.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /c /Ox /threads /recursive /libs:dll /real-size:64 /I. cross.f Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsm.lib Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsm.lib lib /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsm.lib hsmsol.obj hsmdep.obj hsmout.obj hsmgeo.obj hsmabd.obj hsmeqn.obj hsmbc.obj hsmprj.obj hsmren.obj hsmre1.obj hsmrfm.obj hsmbb2.obj hsmglr.obj ludcmp.obj sbsolve.obj atanc.obj bmdump.obj cross.obj Microsoft (R) Library Manager Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. ifort /Ox /threads /real-size:64 /I. hsmrun.f C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsm.lib /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\hsmrun.exe /link /NODEFAULTLIB:MSVCRT Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. -out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\hsmrun.exe -subsystem:console /NODEFAULTLIB:MSVCRT hsmrun.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsm.lib del *.f *.inc cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\hsm\src cd .. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll /dll /def:hsmAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmUtils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmAdj.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\rcm.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\genrcmi.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib hsm.lib /NODEFAULTLIB:LIBCMT Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\hsmAIM.dll;2 cd .. cd skeleton nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils skeletonAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\skeletonAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. skeletonAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll /dll /def:skeletonAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\skeletonAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll;2 cd .. cd su2 nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\meshWriter\su2Writer /I..\utils su2AIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2AIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2AIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2Utils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2Utils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2Utils.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2_4_Cardinal.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_4_Cardinal.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2_4_Cardinal.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2_5_Raven.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_5_Raven.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2_5_Raven.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2_6_Falcon.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_6_Falcon.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2_6_Falcon.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2_7_Blackbird.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_7_Blackbird.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2_7_Blackbird.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils su2_8_Harrier.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_8_Harrier.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. su2_8_Harrier.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll /dll /def:su2AIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2AIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2Utils.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_4_Cardinal.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_5_Raven.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_6_Falcon.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_7_Blackbird.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\su2_8_Harrier.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\su2AIM.dll;2 cd .. cd tacs nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils tacsAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tacsAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. tacsAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll /dll /def:tacsAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tacsAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tacsAIM.dll;2 cd .. cd xfoil nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils xfoilAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\xfoilAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. xfoilAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll /dll /def:xfoilAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\xfoilAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\xfoilAIM.dll;2 cd .. cd mses nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils msesAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. msesAIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils msesUtils.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesUtils.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. msesUtils.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll /dll /def:msesAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesUtils.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\msesAIM.dll;2 cd .. cd interference nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I. cloudFns.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cloudFns.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. cloudFns.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include interferenceAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\interferenceAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. interferenceAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll /dll /def:interferenceAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\interferenceAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\cloudFns.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\interferenceAIM.dll;2 cd .. cd aflr2 nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.exe Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.exe cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.exe /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.obj /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src aflr2_version.c /link /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr2c.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr2_version.c Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.exe /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr2c.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_version.exe cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src -I..\utils aflr2AIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2AIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr2AIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src -I..\utils aflr2_Interface.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_Interface.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr2_Interface.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll /dll /def:aflr2AIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2AIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr2_Interface.obj /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib AFLR.lib /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib legacy_stdio_definitions.lib /ignore:4078 /ignore:4217 Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr2AIM.dll;2 cd .. cd aflr3 nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.exe Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.exe cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.exe /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.obj /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src aflr3_version.c /link /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr3.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr3_version.c Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.exe /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr3.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_version.exe 16.32.49 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src aflr3AIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3AIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr3AIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\utils -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src aflr3_Interface.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_Interface.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr3_Interface.c cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /W0 /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ /Dstrcasecmp=stricmp -D_ENABLE_EGADS_ -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4 C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\EG_getEffBodyTopos.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_check_tess_coord.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_check_tess_ordering.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_get_bedge_coord.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_get_edge_spacing.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_get_faceOrder.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_get_face_spacing.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_get_surf_grid.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_create_tess.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_tess_to_dgeom.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_aflr4_version.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_auto_cad_geom_setup.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_add_attr.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_add_ff.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_add_ret_attr.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_bodyFlag.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_check_bc.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_data_cleanup.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_edgeData.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_edgeFace.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_edit.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_faceEdge.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_faceFace.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_faceFlag.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_faceLoop.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_file_read.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_file_write.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_idef2idef.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_loopEdge.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_nodeData.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_reset_attr.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_setup.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_write_topo_data.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_curv_at_uv.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_edge_arclen.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_norm_at_uv.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_uv_at_t.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_uv_at_xyz.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_uv_bounds.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_xyz_at_u.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_eval_xyz_at_uv.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_face_node_map.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_cad_geom_faceMatch.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_data.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\egads_aflr4\egads_mzone.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. EG_getEffBodyTopos.c egads_aflr4_check_tess_coord.c egads_aflr4_check_tess_ordering.c egads_aflr4_get_bedge_coord.c egads_aflr4_get_edge_spacing.c egads_aflr4_get_faceOrder.c egads_aflr4_get_face_spacing.c egads_aflr4_get_surf_grid.c egads_aflr4_create_tess.c egads_aflr4_tess_to_dgeom.c egads_aflr4_version.c egads_auto_cad_geom_setup.c egads_cad_geom_add_attr.c egads_cad_geom_add_ff.c egads_cad_geom_add_ret_attr.c egads_cad_geom_bodyFlag.c egads_cad_geom_check_bc.c egads_cad_geom_data_cleanup.c egads_cad_geom_edgeData.c egads_cad_geom_edgeFace.c Generating Code... Compiling... egads_cad_geom_edit.c egads_cad_geom_faceEdge.c egads_cad_geom_faceFace.c egads_cad_geom_faceFlag.c egads_cad_geom_faceLoop.c egads_cad_geom_file_read.c egads_cad_geom_file_write.c egads_cad_geom_idef2idef.c egads_cad_geom_loopEdge.c egads_cad_geom_nodeData.c egads_cad_geom_reset_attr.c egads_cad_geom_setup.c egads_cad_geom_write_topo_data.c egads_eval_curv_at_uv.c egads_eval_edge_arclen.c egads_eval_norm_at_uv.c egads_eval_uv_at_t.c egads_eval_uv_at_xyz.c egads_eval_uv_bounds.c egads_eval_xyz_at_u.c Generating Code... Compiling... egads_eval_xyz_at_uv.c egads_face_node_map.c egads_cad_geom_faceMatch.c egads_data.c egads_mzone.c Generating Code... cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /W0 /Fo"C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj"\ /Dstrcasecmp=stricmp -D_ENABLE_EGADS_ -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\aflr43 C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\aflr43\aflr43_bc_mod.c C:\Users\jenkins\AFLR\aflr_lib_11.5.9\src\aflr43\aflr43_bc_reset.c Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr43_bc_mod.c aflr43_bc_reset.c Generating Code... del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll /dll /def:aflr3AIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3AIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr3_Interface.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_getEffBodyTopos.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_check_tess_coord.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_check_tess_ordering.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_bedge_coord.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_edge_spacing.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_faceOrder.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_face_spacing.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_surf_grid.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_create_tess.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_tess_to_dgeom.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_auto_cad_geom_setup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_ff.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_ret_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_bodyFlag.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_check_bc.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_data_cleanup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edgeData.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edgeFace.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edit.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceEdge.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceFace.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceFlag.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceLoop.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_file_read.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_file_write.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_idef2idef.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_loopEdge.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_nodeData.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_reset_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_setup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_write_topo_data.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_curv_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_edge_arclen.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_norm_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_at_t.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_at_xyz.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_bounds.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_xyz_at_u.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_xyz_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_face_node_map.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceMatch.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_data.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_mzone.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr43_bc_mod.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr43_bc_reset.obj /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib AFLR.lib /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib legacy_stdio_definitions.lib /ignore:4078 /ignore:4217 Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr3AIM.dll;2 cd .. cd aflr4 nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.exe Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.exe cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.exe /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.obj /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src aflr4_version.c /link /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr4.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr4_version.c Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.exe /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib aflr4.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_version.exe cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src -I..\utils aflr4AIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4AIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr4AIM.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\AFLR\aflr_lib_11.5.9\src -I..\utils aflr4_Interface.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_Interface.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aflr4_Interface.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll /dll /def:aflr4AIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4AIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aflr4_Interface.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\EG_getEffBodyTopos.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_check_tess_coord.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_check_tess_ordering.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_bedge_coord.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_edge_spacing.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_faceOrder.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_face_spacing.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_get_surf_grid.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_create_tess.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_tess_to_dgeom.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_aflr4_version.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_auto_cad_geom_setup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_ff.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_add_ret_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_bodyFlag.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_check_bc.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_data_cleanup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edgeData.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edgeFace.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_edit.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceEdge.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceFace.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceFlag.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceLoop.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_file_read.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_file_write.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_idef2idef.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_loopEdge.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_nodeData.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_reset_attr.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_setup.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_write_topo_data.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_curv_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_edge_arclen.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_norm_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_at_t.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_at_xyz.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_uv_bounds.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_xyz_at_u.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_eval_xyz_at_uv.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_face_node_map.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_cad_geom_faceMatch.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_data.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\egads_mzone.obj /LIBPATH:C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\lib AFLR.lib /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib legacy_stdio_definitions.lib /ignore:4078 /ignore:4217 Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\aflr4AIM.dll;2 xcopy /Q /Y C:\Users\jenkins\AFLR\aflr_lib_11.5.9\WIN64\bin\AFLR.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib 1 File(s) copied cd .. cd awave nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils awaveAIM.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awaveAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. awaveAIM.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll /dll /def:awaveAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awaveAIM.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\awaveAIM.dll;2 ifort /c /Ox /threads /recursive /libs:dll awavemod.f /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awave.obj Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. ifort /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\awave.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awave.obj Intel(R) Fortran Intel(R) 64 Compiler Classic for applications running on Intel(R) 64, Version 2021.10.0 Build 20230609_000000 Copyright (C) 1985-2023 Intel Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. -out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\awave.exe -subsystem:console C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awave.obj cd .. cd tetgen nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /I..\utils tetgenAIM.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgenAIM.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. tetgenAIM.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /DTETLIBRARY /IC:\Users\jenkins\tetgen\tetgen1.6.0 /I..\utils tetgen_Interface.cpp /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgen_Interface.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. tetgen_Interface.cpp cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /W0 -DTETLIBRARY C:\Users\jenkins\tetgen\tetgen1.6.0\tetgen.cxx /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgen.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. tetgen.cxx cl /c /Ob2 /Oi /Ot /Oy /MD /EHsc /GR /D_CRT_SECURE_NO_DEPRECATE /Od /W0 C:\Users\jenkins\tetgen\tetgen1.6.0\predicates.cxx /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\predicates.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. predicates.cxx del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll /dll /def:tetgenAIM.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgenAIM.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgen_Interface.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\tetgen.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\predicates.obj /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\tetgenAIM.dll;2 cd .. cd custom nmake -f Nmakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd .. cd ..\test nmake -f aim.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers aim.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aim.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aim.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\aim.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aim.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\aim.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aim.obj copy /Y testingAIM.csm C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\testingAIM.csm 1 file(s) copied. nmake -f autoExec.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers autoExec.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\autoExec.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. autoExec.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\autoExec.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\autoExec.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\autoExec.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\autoExec.obj nmake -f newPhase.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include newPhase.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\newPhase.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. newPhase.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\newPhase.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\newPhase.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\newPhase.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\newPhase.obj nmake -f basic.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include basic.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\basic.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. basic.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\basic.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\basic.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\basic.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\basic.obj nmake -f geomIn.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include geomIn.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\geomIn.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. geomIn.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\geomIn.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\geomIn.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\geomIn.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\geomIn.obj nmake -f utilsTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers aimTransferUtilTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimTransferUtilTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aimTransferUtilTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\aimTransferUtilTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimTransferUtilTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\aimTransferUtilTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aimTransferUtilTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\aim\utils -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers miscUtilsTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\miscUtilsTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. miscUtilsTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\miscUtilsTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\miscUtilsTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\miscUtilsTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\miscUtilsTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -I..\aim\utils -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers vlmUtilsTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vlmUtilsTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. vlmUtilsTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vlmUtilsTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vlmUtilsTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vlmUtilsTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib utils.lib aimUtil.lib ocsm.lib egads.lib udunits2.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vlmUtilsTest.obj nmake -f vVS.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers vVS.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vVS.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. vVS.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vVS.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib wsserver.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\vVS.obj echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe;1 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\vVS.exe;1 cd ..\examples nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\csmData mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\csmData if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\pyCAPS mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\pyCAPS if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\corsairlite mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\corsairlite if not exist C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest mkdir C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\csmData xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\csmData\*.* /Q /Y 36 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\pyCAPS xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\pyCAPS\*.* /Q /Y 121 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\corsairlite xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\corsairlite\* /Q /Y /E /S 25 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\regressionTest\*.* /Q /Y 2 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\cCAPS nmake -f avlTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include avlTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. avlTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\avlTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\avlTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\avlTest.obj nmake -f awaveTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include awaveTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awaveTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. awaveTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\awaveTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awaveTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\awaveTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\awaveTest.obj nmake -f frictionTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include frictionTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\frictionTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. frictionTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\frictionTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\frictionTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\frictionTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\frictionTest.obj nmake -f fun3d.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include fun3dTetgenTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dTetgenTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fun3dTetgenTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/fun3dTetgenTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dTetgenTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/fun3dTetgenTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dTetgenTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include aeroelasticTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aeroelasticTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. aeroelasticTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/aeroelasticTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aeroelasticTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/aeroelasticTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\aeroelasticTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include fun3dAFLR2Test.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dAFLR2Test.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. fun3dAFLR2Test.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/fun3dAFLR2Test.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dAFLR2Test.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/fun3dAFLR2Test.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\fun3dAFLR2Test.obj nmake -f hsm.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include hsmTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include hsmSimplePlateTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmSimplePlateTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmSimplePlateTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmSimplePlateTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmSimplePlateTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmSimplePlateTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmSimplePlateTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include hsmCantileverPlateTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmCantileverPlateTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmCantileverPlateTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmCantileverPlateTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmCantileverPlateTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmCantileverPlateTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmCantileverPlateTest.obj cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include hsmJoinedPlateTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmJoinedPlateTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. hsmJoinedPlateTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmJoinedPlateTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmJoinedPlateTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\hsmJoinedPlateTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\hsmJoinedPlateTest.obj nmake -f interferenceTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include interferenceTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\interferenceTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. interferenceTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\interferenceTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\interferenceTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\interferenceTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\interferenceTest.obj nmake -f msesTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include msesTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. msesTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\msesTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\msesTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\msesTest.obj nmake -f mystran.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include mystranTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. mystranTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/mystranTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS/mystranTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\mystranTest.obj nmake -f pointwiseTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include pointwiseTest.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\pointwiseTest.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. pointwiseTest.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\pointwiseTest.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\pointwiseTest.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\pointwiseTest.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\pointwiseTest.obj cd ..\Slugs\src nmake -f NMakefile Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include\winhelpers Slugs.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Slugs.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Slugs.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include Fitter.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Fitter.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Fitter.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include RedBlackTree.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\RedBlackTree.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. RedBlackTree.c cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include Tessellate.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Tessellate.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Tessellate.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\Slugs.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Slugs.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Fitter.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\RedBlackTree.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Tessellate.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib wsserver.lib z.lib egads.lib ws2_32.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\bin\Slugs.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib wsserver.lib z.lib egads.lib ws2_32.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Slugs.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Fitter.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\RedBlackTree.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\Tessellate.obj cd ..\.. Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\skeletonAIM.dll' is up-to-date Build training sessions Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 -IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include template_avl.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\template_avl.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. template_avl.c cl /FeC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\template_avl.exe C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\template_avl.obj /link /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\test\template_avl.exe /LIBPATH:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib /LIBPATH:C:\Users\jenkins\OpenCASCADE-7.6.0\win64\vc14\lib caps.lib egads.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\template_avl.obj Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Compiling serveESP Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timCapsMode.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timCapsMode.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timCapsMode.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timCapsMode.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\capsMode.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timFlowchart.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timFlowchart.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timFlowchart.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timFlowchart.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\flowchart.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include /IC:\Users\jenkins\ESP_Python-3.11.6\include timPyscript.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPyscript.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timPyscript.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll /dll /def:timPyscript.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timPyscript.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib C:\Users\jenkins\ESP_Python-3.11.6\libs\python311.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\pyscript.dll;2 cl /c /Ox /MD /D_CRT_SECURE_NO_DEPRECATE /DWNT /DNDEBUG /D_CONSOLE /DWIN32 /DREVISION=7.6 /D_OCC64 /IC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\include timViewer.c /FoC:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timViewer.obj Microsoft (R) C/C++ Optimizing Compiler Version 19.29.30153 for x64 Copyright (C) Microsoft Corporation. All rights reserved. timViewer.c del C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.exp Could Not Find C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll link /out:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll /dll /def:tim.def C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\obj\timViewer.obj C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\caps.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\ocsm.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\wsserver.lib C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\egads.lib Microsoft (R) Incremental Linker Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. Creating library C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.lib and object C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.exp echo /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll;2 /manifest C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll.manifest /outputresource:C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\lib\viewer.dll;2 C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\applyTparams.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\biconvex.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\boxudc.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\capsHeader.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\capsViews.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\combine.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\contains.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\diamond.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\duct.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\expressions.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\flapz.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\fuselage.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\gen_rot.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\glovesFuse.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\glovesVtail.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\glovesWing.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\overlaps.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\popupz.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\replicate.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\splitEdges.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\spoilerz.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\strut.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\swap.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewAstros.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewAvl.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewConcept.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewMasstran.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewSansLIP.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewSkinStructure.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewSu2Inviscid.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\viewSu2Viscous.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\wake.udc C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\OpenCSM\trunk\udc\wing.udc 33 File(s) copied Build training sessions Add training sessions to PATH Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\csmData xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\csmData\*.* /Q /Y 36 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\pyCAPS xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\pyCAPS\*.* /Q /Y 121 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\corsairlite xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\corsairlite\* /Q /Y /E /S 25 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest xcopy C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\regressionTest\*.* /Q /Y 2 File(s) copied cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\examples\cCAPS nmake -f avlTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\avlTest.exe' is up-to-date nmake -f awaveTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\awaveTest.exe' is up-to-date nmake -f frictionTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\frictionTest.exe' is up-to-date nmake -f fun3d.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. nmake -f hsm.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. nmake -f interferenceTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\interferenceTest.exe' is up-to-date nmake -f msesTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\msesTest.exe' is up-to-date nmake -f mystran.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\mystranTest.exe' is up-to-date nmake -f pointwiseTest.mak Microsoft (R) Program Maintenance Utility Version 14.29.30153.0 Copyright (C) Microsoft Corporation. All rights reserved. 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\cCAPS\pointwiseTest.exe' is up-to-date cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest bash.exe -ex execute_CTestRegression.sh LINEARAERO + stat=0 + notExpectedTests= + notRun= + LOGFILENAME=cCAPSlog.txt + curDir=regressionTest + regTestDir=/c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest + [[ regressionTest != \r\e\g\r\e\s\s\i\o\n\T\e\s\t ]] + [[ ! -d ../csmData ]] + [[ ! -d ../cCAPS ]] + LOGFILE=/c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt + rm -f /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt + touch /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt + cd ../cCAPS + TYPE=ALL + testsRan=0 + [[ LINEARAERO != '' ]] + TYPE=LINEARAERO + [[ Windows_NT == \W\i\n\d\o\w\s\_\N\T ]] + EXT=dll + [[ LINEARAERO == \M\I\N\I\M\A\L ]] + [[ LINEARAERO == \A\L\L ]] + [[ LINEARAERO == \L\I\N\E\A\R\A\E\R\O ]] + echo 'Running.... LINEARAERO c-Tests' Running.... LINEARAERO c-Tests ++ which avl + [[ /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/avl != '' ]] + expectCSuccess ./avlTest 0 + echo + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt + echo ================================================= + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt ================================================= + local status + set -x + echo './avlTest test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt ./avlTest test; + ./avlTest 0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt Attention: avlTest is hard coded to look for ../csmData/avlWingTail.csm Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice control surface data VLM control surface name - WingRightLE VLM control surface name - WingRightTE VLM control surface name - Tail Done getting vortex lattice control surface data Getting vortex lattice surface data VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Wing (ID = 0) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Writing surface - Vertical_Tail (ID = 1) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Running AVL! Value of Cltot = 0.619913 StripForces Wing = {"Xle":[1.565221892029e+00,1.512117367810e+00,1.409527304938e+00,1.264443046659e+00,1.086751845411e+00,8.885630629098e-01,6.833829371601e-01,4.851941546545e-01,3.075029533974e-01,1.624186951053e-01,5.982863221714e-02,6.724107980270e-03,6.724107971058e-03,5.982863219013e-02,1.624186950623e-01,3.075029533414e-01,4.851941545893e-01,6.833829370902e-01,8.885630628399e-01,1.086751845346e+00,1.264443046603e+00,1.409527304895e+00,1.512117367783e+00,1.565221892020e+00],"Yle":[-3.856416046770e+00,-3.725576361740e+00,-3.472813499993e+00,-3.115352832843e+00,-2.677554714026e+00,-2.189254361841e+00,-1.683728638332e+00,-1.195428286135e+00,-7.576301672945e-01,-4.001695001132e-01,-1.474066383261e-01,-1.656695325269e-02,1.656695322999e-02,1.474066382596e-01,4.001695000074e-01,7.576301671565e-01,1.195428285974e+00,1.683728638159e+00,2.189254361668e+00,2.677554713865e+00,3.115352832706e+00,3.472813499887e+00,3.725576361674e+00,3.856416046747e+00],"Zle":[2.486597711706e-01,2.402232939480e-01,2.239252714835e-01,2.008763870743e-01,1.726473841027e-01,1.411620224705e-01,1.085659775407e-01,7.708061590764e-02,4.885161293456e-02,2.580272852328e-02,9.504706056265e-03,1.068228830823e-03,1.068228829360e-03,9.504706051974e-03,2.580272851645e-02,4.885161292566e-02,7.708061589728e-02,1.085659775295e-01,1.411620224593e-01,1.726473840924e-01,2.008763870654e-01,2.239252714767e-01,2.402232939437e-01,2.486597711692e-01],"Chord":[9.710071581587e-01,9.928137666999e-01,1.034940899447e+00,1.094517661923e+00,1.167483996219e+00,1.248867367237e+00,1.333121632734e+00,1.414505003754e+00,1.487471338054e+00,1.547048100535e+00,1.589175233289e+00,1.610981841837e+00,1.610981841841e+00,1.589175233300e+00,1.547048100553e+00,1.487471338077e+00,1.414505003781e+00,1.333121632763e+00,1.248867367266e+00,1.167483996246e+00,1.094517661946e+00,1.034940899465e+00,9.928137667110e-01,9.710071581625e-01],"Area":[6.420432739224e-02,1.924649501823e-01,3.191588402418e-01,4.398794051499e-01,5.463997379092e-01,6.272332670617e-01,6.695492724342e-01,6.620092145623e-01,5.978048871833e-01,4.770843222898e-01,3.080744268775e-01,1.065203328294e-01,1.065203327570e-01,3.080744268129e-01,4.770843222394e-01,5.978048871514e-01,6.620092145502e-01,6.695492724407e-01,6.272332670835e-01,5.463997379421e-01,4.398794051895e-01,3.191588402846e-01,1.924649502262e-01,6.420432743628e-02],"c_cl":[1.751976980131e-01,4.816388142980e-01,7.134545983425e-01,8.955798774854e-01,1.045275116632e+00,1.165642609066e+00,1.251488483106e+00,1.294909342036e+00,1.290147495293e+00,1.237589733955e+00,1.147354354590e+00,1.069716379938e+00,1.027204841580e+00,9.123069911140e-01,8.271224835189e-01,7.465072383829e-01,6.622506856527e-01,5.718077594720e-01,4.773770050905e-01,3.839108464455e-01,2.965810831881e-01,2.166269422082e-01,1.372747954618e-01,4.847522879861e-02],"ai":[2.423376448062e-01,1.891573605670e-01,1.387726073610e-01,1.136377561111e-01,1.056109957988e-01,1.077519869781e-01,1.163918473304e-01,1.297918603655e-01,1.465983278745e-01,1.624995174599e-01,1.707158095744e-01,1.656351191924e-01,-7.833998870069e-02,-4.190817556550e-02,-1.699095118252e-02,-7.589503463269e-04,7.958849673324e-03,1.019416065192e-02,8.688915578664e-03,6.053380335365e-03,5.120395027034e-03,9.296755297873e-03,2.004804046071e-02,3.330492577589e-02],"cl_norm":[2.044051829732e-01,5.494672225944e-01,7.808579037671e-01,9.268407130709e-01,1.014078158136e+00,1.057019341176e+00,1.062951411332e+00,1.036333388588e+00,9.816462634657e-01,9.051794884122e-01,8.167547094734e-01,7.499676468301e-01,7.211772113982e-01,6.503467495440e-01,6.057660560789e-01,5.686988847409e-01,5.305932247986e-01,4.861412346272e-01,4.332732553839e-01,3.727603475171e-01,3.071901673660e-01,2.373206031159e-01,1.568074209169e-01,5.666485024198e-02],"cl":[1.803741931756e-01,4.848688546459e-01,6.890559834545e-01,8.178762563197e-01,8.948575908405e-01,9.327503738523e-01,9.379850374388e-01,9.144963748400e-01,8.662385668552e-01,7.987616435483e-01,7.207325646090e-01,6.617973538495e-01,6.363916792641e-01,5.738884333905e-01,5.345488897546e-01,5.018395375447e-01,4.682137871232e-01,4.289878157188e-01,3.823352848870e-01,3.289366049983e-01,2.710752133784e-01,2.094198967381e-01,1.383722840117e-01,5.000302093687e-02],"cd":[4.708816796028e-03,1.893013552462e-02,2.388458719217e-02,2.809788812561e-02,3.450496926232e-02,4.310977683936e-02,5.296690620751e-02,6.273588035908e-02,7.092746653695e-02,7.623132904850e-02,7.793919402374e-02,1.330641046361e-01,7.642533954139e-02,1.575280561794e-02,1.020926164300e-02,5.734996040044e-03,2.453990236882e-03,7.034156944422e-05,-1.681061755697e-03,-2.904871637687e-03,-3.696799546922e-03,-4.291551637882e-03,-4.755989795807e-03,-4.178738547375e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-6.175122770635e-02,-1.541367450249e-01,-1.990020049078e-01,-2.179523703798e-01,-2.259241556000e-01,-2.291785023832e-01,-2.301045091168e-01,-2.293937884749e-01,-2.266765134794e-01,-2.205756980543e-01,-2.089282623641e-01,-1.947906406100e-01,-1.847119741766e-01,-1.559354818193e-01,-1.355315131375e-01,-1.232795365876e-01,-1.170486694971e-01,-1.141869860843e-01,-1.128288355904e-01,-1.117855412669e-01,-1.094863434133e-01,-1.016126232940e-01,-7.889656776610e-02,-3.215621313961e-02],"cm_LE":[-9.907391078332e-02,-2.553625521061e-01,-3.443180862961e-01,-3.917771248736e-01,-4.170475207536e-01,-4.288879437379e-01,-4.309998082915e-01,-4.249313258859e-01,-4.112512348868e-01,-3.899661415023e-01,-3.610798550199e-01,-3.345295675168e-01,-3.190696575594e-01,-2.776668920570e-01,-2.496150543394e-01,-2.306580335187e-01,-2.170714278267e-01,-2.053105443164e-01,-1.932221818518e-01,-1.798625218874e-01,-1.643057066258e-01,-1.427050164900e-01,-1.051753523064e-01,-4.137433282282e-02],"C.P.x/c":[5.923506801011e-01,5.678936810397e-01,5.388038268097e-01,5.164857534324e-01,5.024693961503e-01,4.957018606561e-01,4.953178888067e-01,5.008416597223e-01,5.116790825907e-01,5.261470832205e-01,5.398832002650e-01,5.443357803971e-01,5.402488831882e-01,5.217174153487e-01,5.035437183300e-01,4.956552889212e-01,4.999897967897e-01,5.161776906017e-01,5.451044281036e-01,5.898391652626e-01,6.538965497758e-01,7.352099770687e-01,8.201760893057e-01,8.930854083837e-01]} Vertical_Tail = {"Xle":[5.481142821257e+00,5.457739875756e+00,5.413224828118e+00,5.351955121359e+00,5.279928261269e+00,5.204194738752e+00,5.132167878660e+00,5.070898171897e+00,5.026383124254e+00,5.002980178746e+00],"Yle":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"Zle":[1.462285642514e+00,1.415479751513e+00,1.326449656236e+00,1.203910242719e+00,1.059856522538e+00,9.083894775049e-01,7.643357573198e-01,6.417963437947e-01,5.527662485071e-01,5.059603574925e-01],"Chord":[7.291641787429e-01,7.525671242437e-01,7.970821718820e-01,8.583518786405e-01,9.303787387310e-01,1.006112261248e+00,1.078139121340e+00,1.139408828103e+00,1.183923875746e+00,1.207326821254e+00],"Area":[1.727730179136e-02,5.174997687051e-02,8.537019049526e-02,1.158415604078e-01,1.391867381176e-01,1.505166423044e-01,1.455036346588e-01,1.220345306258e-01,8.141205112924e-02,2.860720599220e-02],"c_cl":[4.143502484418e-02,1.146121890397e-01,1.669674480704e-01,2.000258625574e-01,2.165069436647e-01,2.173612378313e-01,2.020982864238e-01,1.687203348324e-01,1.143884794128e-01,4.073751989356e-02],"ai":[2.065296924524e-01,1.849180223915e-01,1.591285664757e-01,1.456224964407e-01,1.435231644006e-01,1.506386553619e-01,1.666466052405e-01,1.914179167692e-01,2.193221173426e-01,2.365321328628e-01],"cl_norm":[6.579957348175e-02,1.763463053600e-01,2.425545992661e-01,2.698370559984e-01,2.694590983036e-01,2.501591871286e-01,2.170544160378e-01,1.714623014102e-01,1.118766125248e-01,3.907064104103e-02],"cl":[5.682537081788e-02,1.522949719002e-01,2.094733190132e-01,2.330348048801e-01,2.327083956798e-01,2.160407403860e-01,1.874510278160e-01,1.480770823176e-01,9.661810337317e-02,3.374191575671e-02],"cd":[4.670566079259e-03,1.374698956983e-02,1.845844898550e-02,2.032218684722e-02,2.072187092669e-02,2.023884851594e-02,1.896705322928e-02,1.657142171116e-02,1.222733795464e-02,5.106244760906e-03],"cdv":[0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00,0.000000000000e+00],"cm_c/4":[-3.303465544546e-02,-8.761746958841e-02,-1.194746602282e-01,-1.341488123562e-01,-1.380350789961e-01,-1.339349413679e-01,-1.218867053323e-01,-1.002593790934e-01,-6.716156843018e-02,-2.373448304332e-02],"cm_LE":[-4.232877133358e-02,-1.126299441676e-01,-1.539951982649e-01,-1.724118490115e-01,-1.757829360722e-01,-1.683239687782e-01,-1.510824211715e-01,-1.228726806386e-01,-8.171902803714e-02,-2.878672165371e-02],"C.P.x/c":[8.313363814436e-01,8.253142634666e-01,8.203574125382e-01,8.256599853196e-01,8.431675932571e-01,8.699522420103e-01,9.002322593393e-01,9.270755982235e-01,9.451240614896e-01,9.534124326092e-01]} real 0m4.503s user 0m0.000s sys 0m0.092s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./avlTest passed (as expected) ============================================= ================================================= + echo './msesTest test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt ./msesTest test; + ./msesTest 0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt Attention: msesTest is hard coded to look for ../csmData/airfoilSection.csm Value of CL = 0.276892 real 0m5.080s user 0m0.015s sys 0m0.061s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./msesTest passed (as expected) ============================================= ================================================= + echo './awaveTest test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt ./awaveTest test; + ./awaveTest 0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 = 1.133363 0.216414 real 0m2.076s user 0m0.015s sys 0m0.093s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./awaveTest passed (as expected) ============================================= ================================================= + echo './frictionTest test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt ./frictionTest test; + ./frictionTest 0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/cCAPSlog.txt Attention: frictionTest is hard coded to look for ../csmData/frictionWingTailFuselage.csm To not make system calls to the friction executable the second command line option may be supplied - 0 = no analysis , >0 run analysis (default). Lifting Surface: Body = 1, units m XLE: 1.571946 -3.872983 0.249728 XTE: 2.536563 -3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 2, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.614012 0.000000 0.002015 Chord: 1.614013 Arc: 3.308635 T/C: 0.127839 Type: Wing Lifting Surface: Body = 3, units m XLE: 1.571946 3.872983 0.249728 XTE: 2.536563 3.872983 0.335335 Chord: 0.968408 Arc: 1.985181 T/C: 0.155975 Type: Wing Lifting Surface: Body = 4, units m XLE: 5.484123 0.000000 1.468246 XTE: 6.210307 0.000915 1.468246 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: VTail Lifting Surface: Body = 5, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.210307 0.001525 0.500000 Chord: 1.210308 Arc: 2.471195 T/C: 0.120035 Type: VTail Lifting Surface: Body = 6, units m XLE: 5.484123 -0.968246 0.500000 XTE: 6.210307 -0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Lifting Surface: Body = 7, units m XLE: 5.484123 0.968246 0.500000 XTE: 6.210307 0.968246 0.500915 Chord: 0.726185 Arc: 1.482717 T/C: 0.120035 Type: HTail Body of Revolution: Body = 8, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 9, units m Arc: 3.714180 Diameter: 1.020621 Type: Fuse Body of Revolution: Body = 10, units m Arc: 2.771209 Diameter: 0.645497 Type: Fuse Body of Revolution: Body = 11, units m Arc: 1.013945 Diameter: 0.322749 Type: Fuse Body of Revolution: Body = 12, units m Arc: 0.101394 Diameter: 0.032275 Type: Fuse Number of sections 4, number of revolution sections 1 Number of Mach-Altitude cases = 2 Running FRICTION! Value of CDfric = 0.009900 Value of CDfric = 0.009190 real 0m1.566s user 0m0.030s sys 0m0.108s + status=0 + set +x ============================================= CAPS verification (using c-executables) case ./frictionTest passed (as expected) ============================================= All tests pass! cd C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\ESP\WIN64\examples\regressionTest bash.exe -ex execute_PyTestRegression.sh LINEARAERO + stat=0 + notExpectedTests= + notRun= + LOGFILENAME=pyCAPSlog.txt + echo + echo ================================================= ================================================= ++ which python + echo 'Using python : /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/venv/Scripts/python' Using python : /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/venv/Scripts/python + echo ================================================= ================================================= + echo + curDir=regressionTest + regTestDir=/c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest + [[ regressionTest != \r\e\g\r\e\s\s\i\o\n\T\e\s\t ]] + [[ ! -d ../csmData ]] + [[ ! -d ../pyCAPS ]] + LOGFILE=/c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt + rm -f /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt + touch /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt + cd ../pyCAPS + TYPE=ALL + testsRan=0 + '[' LINEARAERO '!=' '' ']' + TYPE=LINEARAERO + '[' Windows_NT == Windows_NT ']' + EXT=dll + '[' LINEARAERO == MINIMAL ']' + [[ LINEARAERO == \L\I\N\E\A\R\A\E\R\O ]] + echo 'Running.... LINEARAERO PyTests' Running.... LINEARAERO PyTests + echo '' ++ command -v avl + [[ -n /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/avl ]] ++ which avl + echo 'avl: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/avl' avl: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/avl + expectPythonSuccess avl_PyTest.py + echo + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt + echo ================================================= + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt ================================================= + local status + set -x + echo 'avl_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 0.0006119078685747062 CYtot -6.284473496001477e-15 CZtot -0.3012861394886067 Cltot -4.781528092304838e-14 Cmtot -0.1945055953450459 Cntot -2.340062347995671e-15 Cl'tot -4.784883814335109e-14 Cn'tot -1.505214228583796e-15 CLtot 0.3012509314150749 CDtot 0.004646353488232777 CDvis 0.0 CLff 0.3009503023520502 CYff -7.714522820740938e-15 CDind 0.004646353488232777 CDff 0.004968969500908224 e 0.9669902146157929 StripForces Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946403, 0.0005114598078396, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080998, -0.0007386538944071, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545] real 0m13.106s user 0m0.031s sys 0m0.046s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_AutoSpan_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 -0.04120015166389612 CYtot -3.068916184157164e-11 CZtot -1.12501878984008 Cltot -9.405559110823051e-11 Cmtot -1.954741199602392 Cntot 9.615680740730314e-12 Cl'tot -9.387344921767787e-11 Cn'tot 1.125571262969869e-11 CLtot 1.12412840223712 CDtot 0.0608281618511102 CDvis 0.0 CLff 1.12310542384883 CYff -3.450246615781293e-11 CDind 0.0608281618511102 CDff -0.2032092696196853 e -0.3293035228294711 real 0m23.622s user 0m0.000s sys 0m0.107s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_DesignSweep_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_DesignSweep_PyTest.py test; + python -u avl_DesignSweep_PyTest.py -outLevel=0 -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444377367 Cl = 0.4382638635253497 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444377367 Cl = 0.4382638635253497 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Cd = 0.01186220444377367 Cl = 0.4382638635253497 Cl[0] = 0.2009337808878334 Cd[0] = 0.002572533601559653 real 7m1.078s user 0m0.062s sys 0m0.327s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_ControlSurf_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 -0.01911479917643712 CYtot 0.0382877040111923 CZtot -0.6203123021542264 Cltot 0.05803020542928865 Cmtot -0.3649415791577314 Cntot -0.0205131754823519 Cl'tot 0.05766336287208883 Cn'tot -0.02152281795715914 CLtot 0.619884226341864 CDtot 0.02993783031518051 CDvis 0.0 CLff 0.6192452092597175 CYff 0.03287079625847402 CDind 0.02993783031518051 CDff 0.02861019822661161 e 0.7130586920544774 real 0m6.816s user 0m0.015s sys 0m0.062s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py passed (as expected) ================================================= ================================================= + echo 'avl_EigenValue_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 0m6.330s user 0m0.015s sys 0m0.108s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt avl_OpenMDAO_3_PyTest.py test; + python -u avl_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Alpha [2.] Beta [3.] Cmtot2 [0.04166298] Alpha [2.] Beta [3.] Cmtot2 [0.04166298] Cmtot2_Alpha [[0.68007176]] Cmtot2_Beta [[0.0008466]] RUNNING THE L-BFGS-B CODE * * * Machine precision = 2.220D-16 N = 2 M = 10 At X0 0 variables are exactly at the bounds At iterate 0 f= 4.16630D-02 |proj g|= 6.80072D-01 Alpha [1.31992824] Beta [2.9991534] Cmtot2 [0.03401795] Cmtot2_Alpha [[0.60837327]] Cmtot2_Beta [[0.0015253]] At iterate 1 f= 3.40180D-02 |proj g|= 6.08373D-01 Alpha [-4.45133036] Beta [2.92288326] Cmtot2 [0.00071304] Cmtot2_Alpha [[0.07860089]] Cmtot2_Beta [[0.00107544]] At iterate 2 f= 7.13044D-04 |proj g|= 7.86009D-02 Alpha [-5.30773219] Beta [2.90057802] Cmtot2 [2.43104345e-05] Cmtot2_Alpha [[0.01420175]] Cmtot2_Beta [[0.00021881]] At iterate 3 f= 2.43104D-05 |proj g|= 1.42017D-02 Alpha [-5.49659696] Beta [2.89526135] Cmtot2 [3.72334447e-08] Cmtot2_Alpha [[0.00055304]] Cmtot2_Beta [[8.7325759e-06]] At iterate 4 f= 3.72334D-08 |proj g|= 5.53036D-04 Alpha [-5.50424967] Beta [2.89504288] Cmtot2 [2.1976458e-12] Cmtot2_Alpha [[4.24793145e-06]] Cmtot2_Beta [[6.71418676e-08]] At iterate 5 f= 2.19765D-12 |proj g|= 4.24793D-06 * * * Tit = total number of iterations Tnf = total number of function evaluations Tnint = total number of segments explored during Cauchy searches Skip = number of BFGS updates skipped Nact = number of active bounds at final generalized Cauchy point Projg = norm of the final projected gradient F = final function value * * * N Tit Tnf Tnint Skip Nact Projg F 2 5 6 5 0 0 4.248D-06 2.198D-12 F = 2.1976458036464751E-012 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-5.50424967] [2.89504288] real 0m40.954s user 0m0.015s sys 0m0.077s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case avl_OpenMDAO_3_PyTest.py passed (as expected) ================================================= awave: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/test/awave ================================================= + echo 'awave_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 = [1.133363, 0.2164137] real 0m4.398s user 0m0.030s sys 0m0.264s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected) ================================================= friction: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/test/friction ================================================= + echo 'friction_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 0m3.821s user 0m0.046s sys 0m0.062s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= mses: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/mses ================================================= + echo 'mses_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt mses_PyTest.py test; + python -u mses_PyTest.py -outLevel=0 -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt Cl = 0.37837910855499307 Cd = 0.0077758584172095266 Cm = 0.005262636995795522 real 0m7.432s user 0m0.015s sys 0m0.077s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected) ================================================= ================================================= + echo 'mses_OpenMDAO_3_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt mses_OpenMDAO_3_PyTest.py test; + python -u mses_OpenMDAO_3_PyTest.py -outLevel=0 + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 [[-0.00011853]] At iterate 4 f= 7.58207D-03 |proj g|= 1.18534D-04 camber [-8.65504264e-05] CD [0.00758207] CD_camber [[-3.88988888e-06]] camber [-0.00020135] CD [0.00758207] CD_camber [[-8.77186624e-05]] At iterate 5 f= 7.58207D-03 |proj g|= 8.77187D-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 8.772D-05 7.582D-03 F = 7.5820684845444393E-003 CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH Optimization Complete ----------------------------------- Optimized values: [-0.00020135] real 0m52.375s user 0m0.015s sys 0m0.124s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case mses_OpenMDAO_3_PyTest.py passed (as expected) ================================================= xfoil: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/bin/xfoil ================================================= + echo 'xfoil_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -outLevel=0 -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL Cl = [1.05475230552407, 1.36488869373582, 1.56607214272039, 2.03059709342836, 1.97271083120867, 1.87307153171894, 1.7605047576027] Cd = [0.0131991208675621, 0.0166540240606034, 0.0200551482563102, 0.0458671341983872, 0.0754256009397174, 0.0994469174482356, 0.127479430988808] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.496044114353196, 0.461377732041153, 0.442376568201411, 0.3612516363932, 0.276104140852458, 0.214381239321316, 0.132988264747733] real 0m7.554s user 0m0.000s sys 0m0.108s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected) ================================================= awave: /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/test/awave ================================================= + echo 'autoLink_Pytest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + python -u autoLink_Pytest.py -outLevel=0 -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/WIN64/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 = [[0.019540190626695868, 0.01741891163486496, 0.01637754544160998, 0.01572340736888129, 0.01529976634123639, 0.015051258605772694, 0.014977771651912143], [0.02003019062669587, 0.017828911634864962, 0.01673754544160998, 0.01606340736888129, 0.01561976634123639, 0.015351258605772694, 0.015267771651912142], [0.020570190626695867, 0.01826891163486496, 0.01712754544160998, 0.016423407368881288, 0.015949766341236387, 0.015671258605772693, 0.015577771651912143], [0.02114019062669587, 0.01873891163486496, 0.017547545441609982, 0.016813407368881286, 0.01631976634123639, 0.016011258605772693, 0.015907771651912143], [0.021770190626695867, 0.01924891163486496, 0.01800754544160998, 0.017233407368881286, 0.01671976634123639, 0.01639125860577269, 0.016267771651912143], [0.02246019062669587, 0.01980891163486496, 0.01850754544160998, 0.017693407368881288, 0.017139766341236387, 0.016801258605772692, 0.01665777165191214], [0.023210190626695867, 0.02041891163486496, 0.01904754544160998, 0.01819340736888129, 0.01760976634123639, 0.01724125860577269, 0.01707777165191214], [0.02425019062669587, 0.02125891163486496, 0.01979754544160998, 0.01887340736888129, 0.01824976634123639, 0.017851258605772694, 0.01765777165191214], [0.025430190626695867, 0.02221891163486496, 0.02063754544160998, 0.019653407368881288, 0.01897976634123639, 0.01853125860577269, 0.018307771651912143], [0.026710190626695867, 0.02324891163486496, 0.021547545441609983, 0.02048340736888129, 0.019759766341236388, 0.019271258605772692, 0.019007771651912142], [0.02810019062669587, 0.02435891163486496, 0.02252754544160998, 0.021383407368881287, 0.02058976634123639, 0.02006125860577269, 0.019757771651912143], [0.029590190626695868, 0.02554891163486496, 0.02357754544160998, 0.02233340736888129, 0.02148976634123639, 0.02090125860577269, 0.02055777165191214]] real 3m3.159s user 0m0.046s sys 0m0.218s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: tsfoil ================================================= All tests pass! ================================================= Legacy Using python : /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/ESP/venv/Scripts/python ================================================= Running.... LINEARAERO PyTests ================================================= + rm -rf avl_PyTest + echo 'avl_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_PyTest.py test; + python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/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 0.0006119078685747062 CYtot -6.284473496001477e-15 CZtot -0.3012861394886067 Cltot -4.781528092304838e-14 Cmtot -0.1945055953450459 Cntot -2.340062347995671e-15 Cl'tot -4.784883814335109e-14 Cn'tot -1.505214228583796e-15 CLtot 0.3012509314150749 CDtot 0.004646353488232777 CDvis 0.0 CLff 0.3009503023520502 CYff -7.714522820740938e-15 CDind 0.004646353488232777 CDff 0.004968969500908224 e 0.9669902146157929 StripForces Wing cl = [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408] Wing cd = [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946403, 0.0005114598078396, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080998, -0.0007386538944071, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545] WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: '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 0m8.517s user 0m0.000s sys 0m0.124s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_AutoSpan_PyTest.py test; + python -u avl_AutoSpan_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Loading AIM ERROR:: (name_not_found) in Branch Brch_000083 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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 [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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 [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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 [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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 [[C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\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 -0.03128890105581925 CYtot -2.11044817062647e-11 CZtot -1.014663137451587 Cltot -6.716953065600433e-11 Cmtot -2.941985138524829 Cntot 8.039869469200626e-12 Cl'tot -6.70189853414633e-11 Cn'tot 9.210914907348648e-12 CLtot 1.01396253272292 CDtot 0.04899244907637161 CDvis 0.0 CLff 1.012753587462351 CYff -2.520318523514418e-11 CDind 0.04899244907637161 CDff -0.08941639978598759 e -0.6085401584755901 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 0m18.981s user 0m0.030s sys 0m0.092s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_DesignSweep_PyTest.py test; + python -u avl_DesignSweep_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.1! Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.15000000000000002! Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.2! Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.25! Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.30000000000000004! Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.35000000000000003! Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.4! Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.45! Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.5! Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.55! Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.7000000000000001! Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.75! Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.8! Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.8500000000000001! Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 5) at Mach number = 0.9500000000000001! Cd = 0.01186220444377367 Cl = 0.4382638635253497 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.1! Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.15000000000000002! Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.2! Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.25! Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.30000000000000004! Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.35000000000000003! Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.4! Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.45! Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.5! Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.55! Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.7000000000000001! Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.75! Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.8! Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.8500000000000001! Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 10) at Mach number = 0.9500000000000001! Cd = 0.01186220444377367 Cl = 0.4382638635253497 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.002572533601559653 Cl = 0.2009337808878334 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.1! Cd = 0.002586364230250734 Cl = 0.2015191856819673 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.15000000000000002! Cd = 0.002609799718825173 Cl = 0.2025075296438165 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.2! Cd = 0.002643444008433759 Cl = 0.2039185811663645 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.25! Cd = 0.002688200921007502 Cl = 0.20578163777955 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.30000000000000004! Cd = 0.002745342060025448 Cl = 0.2081373840564919 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.35000000000000003! Cd = 0.002816610334308529 Cl = 0.2110406736710595 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.4! Cd = 0.002904376657744789 Cl = 0.2145646488021107 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.45! Cd = 0.003011879793053208 Cl = 0.2188068842340149 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.5! Cd = 0.003143602034597162 Cl = 0.2238987294821042 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.55! Cd = 0.003305877285463857 Cl = 0.2300199286492602 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.003507917885484745 Cl = 0.237422386030224 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.00376364367727306 Cl = 0.2464707142750712 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.7000000000000001! Cd = 0.004095167898241434 Cl = 0.2577158067753745 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.75! Cd = 0.004540047408151035 Cl = 0.2720394012169929 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.8! Cd = 0.005168237926869611 Cl = 0.2909701507469994 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.8500000000000001! Cd = 0.0061289307153498 Cl = 0.3174875485942859 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 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 = 0.007818359051296943 Cl = 0.3586078919926844 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Wing, index = 1 Name = Vertical_Tail, index = 2 Getting vortex lattice surface data VLM surface name - Vertical_Tail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control Tail not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Warning: Control WingRightLE not found in controls tuple! Only defaults will be used. Warning: Control WingRightTE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used. Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used. Writing surface - Vertical_Tail (ID = 0) Section 1 of 2 (ID = 0) Control surface 1 of 1 Section 2 of 2 (ID = 1) Control surface 1 of 1 Writing surface - Wing (ID = 1) Section 1 of 3 (ID = 1) Control surface 1 of 2 Control surface 2 of 2 Section 2 of 3 (ID = 0) Control surface 1 of 4 Control surface 2 of 4 Control surface 3 of 4 Control surface 4 of 4 Section 3 of 3 (ID = 2) Control surface 1 of 2 Control surface 2 of 2 Running AVL (sweep angle = 20) at Mach number = 0.9500000000000001! Cd = 0.01186220444377367 Cl = 0.4382638635253497 Cl[0] = 0.2009337808878334 Cd[0] = 0.002572533601559653 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 5m1.342s user 0m0.077s sys 0m0.264s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_ControlSurf_PyTest.py test; + python -u avl_ControlSurf_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/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 -0.01911479917643712 CYtot 0.0382877040111923 CZtot -0.6203123021542264 Cltot 0.05803020542928865 Cmtot -0.3649415791577314 Cntot -0.0205131754823519 Cl'tot 0.05766336287208883 Cn'tot -0.02152281795715914 CLtot 0.619884226341864 CDtot 0.02993783031518051 CDvis 0.0 CLff 0.6192452092597175 CYff 0.03287079625847402 CDind 0.02993783031518051 CDff 0.02861019822661161 e 0.7130586920544774 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m9.711s user 0m0.030s sys 0m0.093s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt avl_EigenValue_PyTest.py test; + python -u avl_EigenValue_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Loading AIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Wing, index = 1 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing mass properties file: caps.mass Parsing MassProp Running AVL Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO EigenValues ('case 1', [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]]) WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: '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 0m7.095s user 0m0.045s sys 0m0.077s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt awave_PyTest.py test; + python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/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 = [1.133363, 0.2164137] 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 0m4.637s user 0m0.015s sys 0m0.046s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt friction_PyTest.py test; + python -u friction_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/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 0m3.968s user 0m0.000s sys 0m0.077s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf xfoil_PyTest + echo 'xfoil_PyTest.py test;' + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt xfoil_PyTest.py test; + python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL Cl = [1.05475230552407, 1.36488869373582, 1.56607214272039, 2.03059709342836, 1.97271083120867, 1.87307153171894, 1.7605047576027] Cd = [0.0131991208675621, 0.0166540240606034, 0.0200551482563102, 0.0458671341983872, 0.0754256009397174, 0.0994469174482356, 0.127479430988808] Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0] Transition location = [0.496044114353196, 0.461377732041153, 0.442376568201411, 0.3612516363932, 0.276104140852458, 0.214381239321316, 0.132988264747733] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m8.770s user 0m0.030s sys 0m0.077s + 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 /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt autoLink_Pytest.py test; + python -u autoLink_Pytest.py -verbosity=0 -workDir=runDirectory -noPlotData + tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.6/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Linked Parameter Mach to analysis frictionAIM input Mach Linked Parameter Mach to analysis awaveAIM input Mach Linked Parameter Mach to analysis avlAIM input Mach Linked Parameter Alpha to analysis awaveAIM input Alpha Linked Parameter Alpha to analysis avlAIM input Alpha Linked Parameter Altitude to analysis frictionAIM input Altitude Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = RightTank, index = 1 Name = LeftTank, index = 2 Name = Wing, index = 3 Name = VertTail, index = 4 Name = HorizTail, index = 5 Name = Fuselage, index = 6 Getting vortex lattice surface data VLM surface name - HorizTail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VertTail No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used Writing surface - HorizTail (ID = 0) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Writing surface - VertTail (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 3 (ID = 0) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 2) Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Body of Revolution: Body = 1, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 2, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 3, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Body of Revolution: Body = 4, units m Arc: 0.526861 Diameter: 0.167705 Type: Store Lifting Surface: Body = 5, units m XLE: 1.361345 -3.354102 0.216271 XTE: 2.196728 -3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 6, units m XLE: 0.000000 0.000000 0.000000 XTE: 1.397775 0.000000 0.001745 Chord: 1.397776 Arc: 2.865362 T/C: 0.127839 Type: Wing Lifting Surface: Body = 7, units m XLE: 1.361345 3.354102 0.216271 XTE: 2.196728 3.354102 0.290409 Chord: 0.838666 Arc: 1.719217 T/C: 0.155975 Type: Wing Lifting Surface: Body = 8, units m XLE: 5.419263 0.000000 1.338525 XTE: 6.048157 0.000792 1.338525 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: VTail Lifting Surface: Body = 9, units m XLE: 5.000000 0.000000 0.500000 XTE: 6.048157 0.001321 0.500000 Chord: 1.048158 Arc: 2.140118 T/C: 0.120035 Type: VTail Lifting Surface: Body = 10, units m XLE: 5.419263 -0.838525 0.500000 XTE: 6.048157 -0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 11, units m XLE: 5.419263 0.000000 0.500000 XTE: 6.048157 0.000000 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Lifting Surface: Body = 12, units m XLE: 5.419263 0.838525 0.500000 XTE: 6.048157 0.838525 0.500792 Chord: 0.628895 Arc: 1.284071 T/C: 0.120035 Type: HTail Body of Revolution: Body = 13, units m Arc: 0.000000 Diameter: 0.000000 Type: Fuse Body of Revolution: Body = 14, units m Arc: 3.216574 Diameter: 0.883883 Type: Fuse Body of Revolution: Body = 15, units m Arc: 2.399938 Diameter: 0.559017 Type: Fuse Body of Revolution: Body = 16, units m Arc: 0.878102 Diameter: 0.279508 Type: Fuse Body of Revolution: Body = 17, units m Arc: 0.087810 Diameter: 0.027951 Type: Fuse Number of sections 5, number of revolution sections 1 Number of Mach-Altitude cases = 1 Running frictionAIM Running avlAIM Cd = [[0.019540190626695868, 0.01741891163486496, 0.01637754544160998, 0.01572340736888129, 0.01529976634123639, 0.015051258605772694, 0.014977771651912143], [0.02003019062669587, 0.017828911634864962, 0.01673754544160998, 0.01606340736888129, 0.01561976634123639, 0.015351258605772694, 0.015267771651912142], [0.020570190626695867, 0.01826891163486496, 0.01712754544160998, 0.016423407368881288, 0.015949766341236387, 0.015671258605772693, 0.015577771651912143], [0.02114019062669587, 0.01873891163486496, 0.017547545441609982, 0.016813407368881286, 0.01631976634123639, 0.016011258605772693, 0.015907771651912143], [0.021770190626695867, 0.01924891163486496, 0.01800754544160998, 0.017233407368881286, 0.01671976634123639, 0.01639125860577269, 0.016267771651912143], [0.02246019062669587, 0.01980891163486496, 0.01850754544160998, 0.017693407368881288, 0.017139766341236387, 0.016801258605772692, 0.01665777165191214], [0.023210190626695867, 0.02041891163486496, 0.01904754544160998, 0.01819340736888129, 0.01760976634123639, 0.01724125860577269, 0.01707777165191214], [0.02425019062669587, 0.02125891163486496, 0.01979754544160998, 0.01887340736888129, 0.01824976634123639, 0.017851258605772694, 0.01765777165191214], [0.025430190626695867, 0.02221891163486496, 0.02063754544160998, 0.019653407368881288, 0.01897976634123639, 0.01853125860577269, 0.018307771651912143], [0.026710190626695867, 0.02324891163486496, 0.021547545441609983, 0.02048340736888129, 0.019759766341236388, 0.019271258605772692, 0.019007771651912142], [0.02810019062669587, 0.02435891163486496, 0.02252754544160998, 0.021383407368881287, 0.02058976634123639, 0.02006125860577269, 0.019757771651912143], [0.029590190626695868, 0.02554891163486496, 0.02357754544160998, 0.02233340736888129, 0.02148976634123639, 0.02090125860577269, 0.02055777165191214]] 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 5m12.733s user 0m0.061s sys 0m0.280s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Legacy Did not run examples for: tsfoil ================================================= All tests pass! (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\regressionTest>set /a "err=0+0+0+0" (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\regressionTest>exit /b 0 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019\CAPS\aim\skeleton>exit 0 [GNU C Compiler (gcc)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.6\CAPS\LINEARAERO\WIN64.2019') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.6,ESPTEST=CAPS/LINEARAERO,ESP_ARCH=WIN64.2019,buildnode=windows10x64 #619'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS