The Jenkins Controller is preparing for shutdown. No new builds can be started.
Skipping 1,295 KB.. Full LogsourceBoxAngle = 0.000000 sourceGrowthFactor = 10.000000 sourcePCDFile = ModelSize = 0 writeGMA = 2.0 assembleTolMult = 2.0 modelOrientIntMeshVolume = 1 Elevate On Export degree = Q1 costThreshold = 0.8 maxIncAngle = 175.0 relax = 0.05 smoothingPasses = 1000 WCNWeight = 0.5 WCNMode = Calculate writeVTU = false CADFile = caps.egads Determining model size from file. Info: Model Size adjusted to 10 Computing maximum DB edge tolerance. Quilt list has 9 entries. Quilt quilt-1: edge tolerance = 2.40432e-07 Quilt quilt-2: edge tolerance = 2.40432e-07 Quilt quilt-3: edge tolerance = 2.40432e-07 Quilt quilt-4: edge tolerance = 5e-08 Quilt quilt-5: edge tolerance = 5e-08 Quilt quilt-6: edge tolerance = 5e-08 Quilt quilt-7: edge tolerance = 5e-08 Quilt quilt-8: edge tolerance = 5e-08 Quilt quilt-9: edge tolerance = 5e-08 Maximum DB edge tolerance = 2.40432e-07 Performing model assembly pass on geometry entities. domParams(MinEdge) defined as 4.808648e-07 due to model assembly tolerance Looking for quilt names in geometry. Quilt list has 9 entries. Quilt list has 9 entries. Original connector list has 15 entries. Minimum connector length = 1 Tolerance = 2.40432e-07 Performing merge on connectors with equal dimensions and common end points. After regular merge, connector list has 15 entries. Updating conData Min Edge Tol: 5.000e-08 on con-5 Max Edge Tol: 2.404e-07 on con-1 Adjusting connector dimensions based on average spacings. Checking dimension for connector 1/15, name = con-1 Checking dimension for connector 2/15, name = con-2 Checking dimension for connector 3/15, name = con-4 Changing dimension for connector 3/15 from 6 to 3 Checking dimension for connector 4/15, name = con-5 Changing dimension for connector 4/15 from 6 to 3 Checking dimension for connector 5/15, name = con-6 Changing dimension for connector 5/15 from 6 to 3 Checking dimension for connector 6/15, name = con-7 Changing dimension for connector 6/15 from 6 to 3 Checking dimension for connector 7/15, name = con-8 Changing dimension for connector 7/15 from 6 to 3 Checking dimension for connector 8/15, name = con-9 Changing dimension for connector 8/15 from 6 to 3 Checking dimension for connector 9/15, name = con-10 Changing dimension for connector 9/15 from 6 to 3 Checking dimension for connector 10/15, name = con-11 Changing dimension for connector 10/15 from 6 to 3 Checking dimension for connector 11/15, name = con-12 Changing dimension for connector 11/15 from 6 to 3 Checking dimension for connector 12/15, name = con-13 Checking dimension for connector 13/15, name = con-15 Checking dimension for connector 14/15, name = con-17 Checking dimension for connector 15/15, name = con-19 Processing spacing values for connector 1/15, name = con-1 Processing spacing values for connector 2/15, name = con-2 Processing spacing values for connector 3/15, name = con-4 Processing spacing values for connector 4/15, name = con-5 Processing spacing values for connector 5/15, name = con-6 Processing spacing values for connector 6/15, name = con-7 Processing spacing values for connector 7/15, name = con-8 Processing spacing values for connector 8/15, name = con-9 Processing spacing values for connector 9/15, name = con-10 Processing spacing values for connector 10/15, name = con-11 Processing spacing values for connector 11/15, name = con-12 Processing spacing values for connector 12/15, name = con-13 Processing spacing values for connector 13/15, name = con-15 Processing spacing values for connector 14/15, name = con-17 Processing spacing values for connector 15/15, name = con-19 Number of unique endpoints = 10 Checking for baffle intersections. Performing Local Proximity Refinement Adjusting connector dimensions based on proximity to other connectors. Proximity test for connector 1/15, con-1. Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799 Proximity test for connector 2/15, con-2. Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799 Proximity test for connector 3/15, con-4. Proximity test for connector 4/15, con-5. Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8 Proximity test for connector 5/15, con-6. Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8 Proximity test for connector 6/15, con-7. Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8 Proximity test for connector 7/15, con-8. Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8 Proximity test for connector 8/15, con-9. Proximity test for connector 9/15, con-10. Proximity test for connector 10/15, con-11. Proximity test for connector 11/15, con-12. Proximity test for connector 12/15, con-13. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 13/15, con-15. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 14/15, con-17. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 15/15, con-19. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Adjusting node spacing from geometry Adjusting connector dimensions based on end spacings. Connector con-1 current dim = 8 Connector con-2 current dim = 8 Connector con-4 current dim = 3 Connector con-5 current dim = 6 Connector con-6 current dim = 6 Connector con-7 current dim = 6 Connector con-8 current dim = 6 Connector con-9 current dim = 3 Connector con-10 current dim = 3 Connector con-11 current dim = 3 Connector con-12 current dim = 3 Connector con-13 current dim = 8 Connector con-15 current dim = 8 Connector con-17 current dim = 8 Connector con-19 current dim = 8 Domain list has 9 entries. Looking for periodic domain attributes from geometry. Tolerance = 2.40432e-07 Number of periodic target domains = 0 Unstructured domain 1 of 9: boundary name = cylinder. Creating boundary name cylinder Unstructured domain 2 of 9: boundary name = cylinder. cylinder already in boundary name list. Unstructured domain 3 of 9: boundary name = cylinder. cylinder already in boundary name list. Unstructured domain 4 of 9: boundary name = farfield. Creating boundary name farfield Unstructured domain 5 of 9: boundary name = farfield. farfield already in boundary name list. Unstructured domain 6 of 9: boundary name = farfield. farfield already in boundary name list. Unstructured domain 7 of 9: boundary name = farfield. farfield already in boundary name list. Unstructured domain 8 of 9: boundary name = farfield. farfield already in boundary name list. Unstructured domain 9 of 9: boundary name = farfield. farfield already in boundary name list. Checking for blunt flag attribute on geometry faces. Performing initialization pass on all unstructured domains. Unstructured domain list for assembly has 9 entries. Structured domain list for assembly has 0 entries. Periodic target domain list for assembly has 0 entries. Creating unstructured block from 9 domains. Block = auto-blk Setting up unstructured block. Retrieving block attributes from geometry. Initializing unstructured block. CAE Solver set to UGRID GeomToMesh finished! Sat Jul 08 2023 10:49:14AM EDT Run Time: 00 Hours 00 Minutes 01 Seconds Pointwise save filename = caps.GeomToMesh.pw Sat Jul 08 2023 10:49:14AM EDT Exporting in UGRID format to file basename = caps.GeomToMesh Mapped 45 / 45 curves to EGADS originals GMA contains 15 edge groups GMA contains 9 face groups Wrote geometry-mesh associativity to caps.GeomToMesh.gma GeomToMesh I/O finished! Sat Jul 08 2023 10:49:15AM EDT Export Time: 00 Hours 00 Minutes 01 Seconds Volume mesh: Number of nodes = 413 Number of elements = 1869 Number of triangles = 348 Number of quadrilatarals = 0 Number of tetrahedrals = 1869 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Body = 1 Number of nodes = 38 Number of elements = 72 Number of tris = 72 Number of quad = 0 Body = 2 Number of nodes = 140 Number of elements = 276 Number of tris = 276 Number of quad = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Writing global Glyph inputs... Writing egads file '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/BoxError/caps.egads'.... .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing global Glyph inputs... Writing egads file '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'.... Running pointwise...... Number of command line arguments = 2 Sat Jul 08 2023 10:49:19AM EDT Pointwise V18.5 Loading user defaults from capsUserDefaults.glf GeomToMesh: Defaults Connector level InitDim = 10 MaxDim = 12 MinDim = 3 TurnAngle = 0.000000 Deviation = 0.000000 SplitAngle = 0.000000 JoinCons = 0 ProxGrowthRate = 1.300000 SourceSpacing = 0 TurnAngleHard = 70.000000 EqualSpacing = 0 Domain level Algorithm = Delaunay FullLayers = 0 MaxLayers = 0 GrowthRate = 1.300000 IsoType = Triangle TRexType = Triangle TRexARLimit = 200.000000 TRexAngleBC = 0.000000 Decay = 0.500000 MinEdge = 0.000000 MaxEdge = 0.000000 Adapt = 0 WallSpacing = 0.000000 StrDomConvertARTrigger = 0.000000 Block level Algorithm = Delaunay VoxelLayers = 3 boundaryDecay = 0.500000 collisionBuffer = 0.500000 maxSkewAngle = 180.000000 TRexSkewDelay = 0 edgeMaxGrowthRate = 1.800000 fullLayers = 0 maxLayers = 0 growthRate = 1.300000 TRexType = TetPyramid volInitialize = 1 General SkipMeshing = 1 CAESolver = UGRID outerBoxScale = 0 sourceBoxLengthScale = 0.000000 sourceBoxDirection = 1.000000 0.000000 0.000000 sourceBoxAngle = 0.000000 sourceGrowthFactor = 10.000000 sourcePCDFile = ModelSize = 0 writeGMA = 2.0 assembleTolMult = 2.0 modelOrientIntMeshVolume = 1 Elevate On Export degree = Q1 costThreshold = 0.8 maxIncAngle = 175.0 relax = 0.05 smoothingPasses = 1000 WCNWeight = 0.5 WCNMode = Calculate writeVTU = false CADFile = caps.egads Determining model size from file. Info: Model Size adjusted to 100 Computing maximum DB edge tolerance. Quilt list has 14 entries. Quilt quilt-1: edge tolerance = 5e-07 Quilt quilt-2: edge tolerance = 5e-07 Quilt quilt-3: edge tolerance = 5e-07 Quilt quilt-4: edge tolerance = 5e-07 Quilt quilt-5: edge tolerance = 5e-07 Quilt quilt-6: edge tolerance = 5e-07 Quilt quilt-7: edge tolerance = 6.19984e-05 Quilt quilt-8: edge tolerance = 6.19984e-05 Quilt quilt-9: edge tolerance = 6.19984e-05 Quilt quilt-10: edge tolerance = 6.19984e-05 Quilt quilt-11: edge tolerance = 6.19984e-05 Quilt quilt-12: edge tolerance = 6.19984e-05 Quilt quilt-13: edge tolerance = 6.19984e-05 Quilt quilt-14: edge tolerance = 6.19984e-05 Maximum DB edge tolerance = 6.19984e-05 Performing model assembly pass on geometry entities. domParams(MinEdge) defined as 1.239969e-04 due to model assembly tolerance Looking for quilt names in geometry. Quilt list has 14 entries. Quilt list has 14 entries. Original connector list has 27 entries. Minimum connector length = 0.00791958 Tolerance = 6.19984e-05 Performing merge on connectors with equal dimensions and common end points. After regular merge, connector list has 27 entries. Updating conData Min Edge Tol: 5.000e-07 on con-1 Max Edge Tol: 6.200e-05 on con-20 Adjusting connector dimensions based on average spacings. Checking dimension for connector 1/27, name = con-1 Checking dimension for connector 2/27, name = con-2 Checking dimension for connector 3/27, name = con-3 Checking dimension for connector 4/27, name = con-4 Checking dimension for connector 5/27, name = con-5 Checking dimension for connector 6/27, name = con-6 Checking dimension for connector 7/27, name = con-7 Checking dimension for connector 8/27, name = con-8 Checking dimension for connector 9/27, name = con-9 Checking dimension for connector 10/27, name = con-11 Checking dimension for connector 11/27, name = con-13 Checking dimension for connector 12/27, name = con-15 Checking dimension for connector 13/27, name = con-16 Changing dimension for connector 13/27 from 10 to 3 Checking dimension for connector 14/27, name = con-17 Changing dimension for connector 14/27 from 10 to 3 Checking dimension for connector 15/27, name = con-18 Changing dimension for connector 15/27 from 10 to 3 Checking dimension for connector 16/27, name = con-19 Changing dimension for connector 16/27 from 10 to 3 Checking dimension for connector 17/27, name = con-20 Changing dimension for connector 17/27 from 10 to 3 Checking dimension for connector 18/27, name = con-21 Changing dimension for connector 18/27 from 10 to 3 Checking dimension for connector 19/27, name = con-22 Checking dimension for connector 20/27, name = con-23 Changing dimension for connector 20/27 from 10 to 3 Checking dimension for connector 21/27, name = con-24 Checking dimension for connector 22/27, name = con-26 Changing dimension for connector 22/27 from 10 to 4 Checking dimension for connector 23/27, name = con-27 Checking dimension for connector 24/27, name = con-29 Changing dimension for connector 24/27 from 10 to 4 Checking dimension for connector 25/27, name = con-31 Checking dimension for connector 26/27, name = con-33 Checking dimension for connector 27/27, name = con-37 Processing spacing values for connector 1/27, name = con-1 Processing spacing values for connector 2/27, name = con-2 Processing spacing values for connector 3/27, name = con-3 Processing spacing values for connector 4/27, name = con-4 Processing spacing values for connector 5/27, name = con-5 Processing spacing values for connector 6/27, name = con-6 Processing spacing values for connector 7/27, name = con-7 Processing spacing values for connector 8/27, name = con-8 Processing spacing values for connector 9/27, name = con-9 Processing spacing values for connector 10/27, name = con-11 Processing spacing values for connector 11/27, name = con-13 Processing spacing values for connector 12/27, name = con-15 Processing spacing values for connector 13/27, name = con-16 Processing spacing values for connector 14/27, name = con-17 Processing spacing values for connector 15/27, name = con-18 Processing spacing values for connector 16/27, name = con-19 Processing spacing values for connector 17/27, name = con-20 Processing spacing values for connector 18/27, name = con-21 Processing spacing values for connector 19/27, name = con-22 Processing spacing values for connector 20/27, name = con-23 Processing spacing values for connector 21/27, name = con-24 Processing spacing values for connector 22/27, name = con-26 Processing spacing values for connector 23/27, name = con-27 Processing spacing values for connector 24/27, name = con-29 Processing spacing values for connector 25/27, name = con-31 Processing spacing values for connector 26/27, name = con-33 Processing spacing values for connector 27/27, name = con-37 Number of unique endpoints = 17 Checking for baffle intersections. Performing Local Proximity Refinement Adjusting connector dimensions based on proximity to other connectors. Proximity test for connector 1/27, con-1. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 2/27, con-2. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 3/27, con-3. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 4/27, con-4. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 5/27, con-5. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 6/27, con-6. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 7/27, con-7. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 8/27, con-8. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 9/27, con-9. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 10/27, con-11. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 11/27, con-13. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 12/27, con-15. Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273 Proximity test for connector 13/27, con-16. Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133 Proximity test for connector 14/27, con-17. Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133 Proximity test for connector 15/27, con-18. Proximity test for connector 16/27, con-19. Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133 Proximity test for connector 17/27, con-20. Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133 Proximity test for connector 18/27, con-21. Proximity test for connector 19/27, con-22. Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244 Proximity test for connector 20/27, con-23. Proximity test for connector 21/27, con-24. Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224 Proximity test for connector 22/27, con-26. Connector dimension changed from 4 to 12, avg. spacing changed from 1.33869 to 0.365097 Proximity test for connector 23/27, con-27. Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354 Proximity test for connector 24/27, con-29. Connector dimension changed from 4 to 12, avg. spacing changed from 1.26705 to 0.34556 Proximity test for connector 25/27, con-31. Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244 Proximity test for connector 26/27, con-33. Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224 Proximity test for connector 27/27, con-37. Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354 Adjusting node spacing from geometry Adjusting connector dimensions based on end spacings. Connector con-1 current dim = 12 Connector con-2 current dim = 12 Connector con-3 current dim = 12 Connector con-4 current dim = 12 Connector con-5 current dim = 12 Connector con-6 current dim = 12 Connector con-7 current dim = 12 Connector con-8 current dim = 12 Connector con-9 current dim = 12 Connector con-11 current dim = 12 Connector con-13 current dim = 12 Connector con-15 current dim = 12 Connector con-16 current dim = 12 Connector con-17 current dim = 12 Connector con-18 current dim = 3 Connector con-19 current dim = 12 Connector con-20 current dim = 12 Connector con-21 current dim = 3 Connector con-22 current dim = 12 Connector con-23 current dim = 3 Connector con-24 current dim = 12 Connector con-26 current dim = 12 Connector con-27 current dim = 12 Connector con-29 current dim = 12 Connector con-31 current dim = 12 Connector con-33 current dim = 12 Connector con-37 current dim = 12 Domain list has 14 entries. Looking for periodic domain attributes from geometry. Tolerance = 6.19984e-05 Number of periodic target domains = 0 Unstructured domain 1 of 14: boundary name = Farfield. Creating boundary name Farfield Unstructured domain 2 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 3 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 4 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 5 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 6 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 7 of 14: boundary name = Wing1. Creating boundary name Wing1 Unstructured domain 8 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 9 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 10 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 11 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 12 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 13 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 14 of 14: boundary name = Wing1. Wing1 already in boundary name list. Checking for blunt flag attribute on geometry faces. Performing initialization pass on all unstructured domains. Unstructured domain list for assembly has 14 entries. Structured domain list for assembly has 0 entries. Periodic target domain list for assembly has 0 entries. Creating unstructured block from 14 domains. Block = auto-blk Setting up unstructured block. Retrieving block attributes from geometry. Initializing unstructured block. CAE Solver set to UGRID GeomToMesh finished! Sat Jul 08 2023 10:49:24AM EDT Run Time: 00 Hours 00 Minutes 05 Seconds Pointwise save filename = caps.GeomToMesh.pw Sat Jul 08 2023 10:49:24AM EDT Exporting in UGRID format to file basename = caps.GeomToMesh Mapped 81 / 81 curves to EGADS originals GMA contains 27 edge groups GMA contains 14 face groups Wrote geometry-mesh associativity to caps.GeomToMesh.gma GeomToMesh I/O finished! Sat Jul 08 2023 10:49:27AM EDT Export Time: 00 Hours 00 Minutes 03 Seconds Volume mesh: Number of nodes = 9590 Number of elements = 53926 Number of triangles = 3008 Number of quadrilatarals = 0 Number of tetrahedrals = 53926 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Body = 1 Number of nodes = 1508 Number of elements = 3008 Number of tris = 3008 Number of quad = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Writing global Glyph inputs... Writing egads file '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'.... Running pointwise...... Number of command line arguments = 2 Sat Jul 08 2023 10:49:28AM EDT Pointwise V18.5 Loading user defaults from capsUserDefaults.glf GeomToMesh: Defaults Connector level InitDim = 6 MaxDim = 8 MinDim = 3 TurnAngle = 0.000000 Deviation = 0.000000 SplitAngle = 0.000000 JoinCons = 0 ProxGrowthRate = 1.300000 SourceSpacing = 0 TurnAngleHard = 70.000000 EqualSpacing = 0 Domain level Algorithm = Delaunay FullLayers = 0 MaxLayers = 0 GrowthRate = 1.300000 IsoType = Triangle TRexType = Triangle TRexARLimit = 200.000000 TRexAngleBC = 0.000000 Decay = 0.500000 MinEdge = 0.000000 MaxEdge = 0.000000 Adapt = 0 WallSpacing = 0.000000 StrDomConvertARTrigger = 0.000000 Block level Algorithm = Delaunay VoxelLayers = 3 boundaryDecay = 0.500000 collisionBuffer = 0.500000 maxSkewAngle = 180.000000 TRexSkewDelay = 0 edgeMaxGrowthRate = 1.800000 fullLayers = 0 maxLayers = 0 growthRate = 1.300000 TRexType = TetPyramid volInitialize = 1 General SkipMeshing = 1 CAESolver = UGRID outerBoxScale = 0 sourceBoxLengthScale = 0.000000 sourceBoxDirection = 1.000000 0.000000 0.000000 sourceBoxAngle = 0.000000 sourceGrowthFactor = 10.000000 sourcePCDFile = ModelSize = 0 writeGMA = 2.0 assembleTolMult = 2.0 modelOrientIntMeshVolume = 1 Elevate On Export degree = Q1 costThreshold = 0.8 maxIncAngle = 175.0 relax = 0.05 smoothingPasses = 1000 WCNWeight = 0.5 WCNMode = Calculate writeVTU = false CADFile = caps.egads Determining model size from file. Info: Model Size adjusted to 100 Computing maximum DB edge tolerance. Quilt list has 14 entries. Quilt quilt-1: edge tolerance = 5e-07 Quilt quilt-2: edge tolerance = 5e-07 Quilt quilt-3: edge tolerance = 5e-07 Quilt quilt-4: edge tolerance = 5e-07 Quilt quilt-5: edge tolerance = 5e-07 Quilt quilt-6: edge tolerance = 5e-07 Quilt quilt-7: edge tolerance = 6.19984e-05 Quilt quilt-8: edge tolerance = 6.19984e-05 Quilt quilt-9: edge tolerance = 6.19984e-05 Quilt quilt-10: edge tolerance = 6.19984e-05 Quilt quilt-11: edge tolerance = 6.19984e-05 Quilt quilt-12: edge tolerance = 6.19984e-05 Quilt quilt-13: edge tolerance = 6.19984e-05 Quilt quilt-14: edge tolerance = 6.19984e-05 Maximum DB edge tolerance = 6.19984e-05 Performing model assembly pass on geometry entities. domParams(MinEdge) defined as 1.239969e-04 due to model assembly tolerance Looking for quilt names in geometry. Quilt list has 14 entries. Quilt list has 14 entries. Original connector list has 27 entries. Minimum connector length = 0.00791958 Tolerance = 6.19984e-05 Performing merge on connectors with equal dimensions and common end points. After regular merge, connector list has 27 entries. Updating conData Min Edge Tol: 5.000e-07 on con-1 Max Edge Tol: 6.200e-05 on con-20 Adjusting connector dimensions based on average spacings. Checking dimension for connector 1/27, name = con-1 Checking dimension for connector 2/27, name = con-2 Checking dimension for connector 3/27, name = con-3 Checking dimension for connector 4/27, name = con-4 Checking dimension for connector 5/27, name = con-5 Checking dimension for connector 6/27, name = con-6 Checking dimension for connector 7/27, name = con-7 Checking dimension for connector 8/27, name = con-8 Checking dimension for connector 9/27, name = con-9 Checking dimension for connector 10/27, name = con-11 Checking dimension for connector 11/27, name = con-13 Checking dimension for connector 12/27, name = con-15 Checking dimension for connector 13/27, name = con-16 Changing dimension for connector 13/27 from 6 to 3 Checking dimension for connector 14/27, name = con-17 Changing dimension for connector 14/27 from 6 to 3 Checking dimension for connector 15/27, name = con-18 Changing dimension for connector 15/27 from 6 to 3 Checking dimension for connector 16/27, name = con-19 Changing dimension for connector 16/27 from 6 to 3 Checking dimension for connector 17/27, name = con-20 Changing dimension for connector 17/27 from 6 to 3 Checking dimension for connector 18/27, name = con-21 Changing dimension for connector 18/27 from 6 to 3 Checking dimension for connector 19/27, name = con-22 Checking dimension for connector 20/27, name = con-23 Changing dimension for connector 20/27 from 6 to 3 Checking dimension for connector 21/27, name = con-24 Checking dimension for connector 22/27, name = con-26 Changing dimension for connector 22/27 from 6 to 3 Checking dimension for connector 23/27, name = con-27 Checking dimension for connector 24/27, name = con-29 Changing dimension for connector 24/27 from 6 to 3 Checking dimension for connector 25/27, name = con-31 Checking dimension for connector 26/27, name = con-33 Checking dimension for connector 27/27, name = con-37 Processing spacing values for connector 1/27, name = con-1 Processing spacing values for connector 2/27, name = con-2 Processing spacing values for connector 3/27, name = con-3 Processing spacing values for connector 4/27, name = con-4 Processing spacing values for connector 5/27, name = con-5 Processing spacing values for connector 6/27, name = con-6 Processing spacing values for connector 7/27, name = con-7 Processing spacing values for connector 8/27, name = con-8 Processing spacing values for connector 9/27, name = con-9 Processing spacing values for connector 10/27, name = con-11 Processing spacing values for connector 11/27, name = con-13 Processing spacing values for connector 12/27, name = con-15 Processing spacing values for connector 13/27, name = con-16 Processing spacing values for connector 14/27, name = con-17 Processing spacing values for connector 15/27, name = con-18 Processing spacing values for connector 16/27, name = con-19 Processing spacing values for connector 17/27, name = con-20 Processing spacing values for connector 18/27, name = con-21 Processing spacing values for connector 19/27, name = con-22 Processing spacing values for connector 20/27, name = con-23 Processing spacing values for connector 21/27, name = con-24 Processing spacing values for connector 22/27, name = con-26 Processing spacing values for connector 23/27, name = con-27 Processing spacing values for connector 24/27, name = con-29 Processing spacing values for connector 25/27, name = con-31 Processing spacing values for connector 26/27, name = con-33 Processing spacing values for connector 27/27, name = con-37 Number of unique endpoints = 17 Checking for baffle intersections. Performing Local Proximity Refinement Adjusting connector dimensions based on proximity to other connectors. Proximity test for connector 1/27, con-1. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 2/27, con-2. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 3/27, con-3. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 4/27, con-4. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 5/27, con-5. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 6/27, con-6. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 7/27, con-7. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 8/27, con-8. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 9/27, con-9. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 10/27, con-11. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 11/27, con-13. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 12/27, con-15. Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286 Proximity test for connector 13/27, con-16. Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495 Proximity test for connector 14/27, con-17. Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495 Proximity test for connector 15/27, con-18. Proximity test for connector 16/27, con-19. Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495 Proximity test for connector 17/27, con-20. Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495 Proximity test for connector 18/27, con-21. Proximity test for connector 19/27, con-22. Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638 Proximity test for connector 20/27, con-23. Proximity test for connector 21/27, con-24. Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638 Proximity test for connector 22/27, con-26. Connector dimension changed from 3 to 8, avg. spacing changed from 2.00803 to 0.573724 Proximity test for connector 23/27, con-27. Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656 Proximity test for connector 24/27, con-29. Connector dimension changed from 3 to 8, avg. spacing changed from 1.90058 to 0.543022 Proximity test for connector 25/27, con-31. Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638 Proximity test for connector 26/27, con-33. Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638 Proximity test for connector 27/27, con-37. Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656 Adjusting node spacing from geometry Adjusting connector dimensions based on end spacings. Connector con-1 current dim = 8 Connector con-2 current dim = 8 Connector con-3 current dim = 8 Connector con-4 current dim = 8 Connector con-5 current dim = 8 Connector con-6 current dim = 8 Connector con-7 current dim = 8 Connector con-8 current dim = 8 Connector con-9 current dim = 8 Connector con-11 current dim = 8 Connector con-13 current dim = 8 Connector con-15 current dim = 8 Connector con-16 current dim = 8 Connector con-17 current dim = 8 Connector con-18 current dim = 3 Connector con-19 current dim = 8 Connector con-20 current dim = 8 Connector con-21 current dim = 3 Connector con-22 current dim = 8 Connector con-23 current dim = 3 Connector con-24 current dim = 8 Connector con-26 current dim = 8 Connector con-27 current dim = 8 Connector con-29 current dim = 8 Connector con-31 current dim = 8 Connector con-33 current dim = 8 Connector con-37 current dim = 8 Domain list has 14 entries. Looking for periodic domain attributes from geometry. Tolerance = 6.19984e-05 Number of periodic target domains = 0 Unstructured domain 1 of 14: boundary name = Farfield. Creating boundary name Farfield Unstructured domain 2 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 3 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 4 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 5 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 6 of 14: boundary name = Farfield. Farfield already in boundary name list. Unstructured domain 7 of 14: boundary name = Wing1. Creating boundary name Wing1 Unstructured domain 8 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 9 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 10 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 11 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 12 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 13 of 14: boundary name = Wing1. Wing1 already in boundary name list. Unstructured domain 14 of 14: boundary name = Wing1. Wing1 already in boundary name list. Checking for blunt flag attribute on geometry faces. Performing initialization pass on all unstructured domains. Unstructured domain list for assembly has 14 entries. Structured domain list for assembly has 0 entries. Periodic target domain list for assembly has 0 entries. Creating unstructured block from 14 domains. Block = auto-blk Setting up unstructured block. Retrieving block attributes from geometry. Initializing unstructured block. CAE Solver set to UGRID GeomToMesh finished! Sat Jul 08 2023 10:49:32AM EDT Run Time: 00 Hours 00 Minutes 04 Seconds Pointwise save filename = caps.GeomToMesh.pw Sat Jul 08 2023 10:49:32AM EDT Exporting in UGRID format to file basename = caps.GeomToMesh Mapped 81 / 81 curves to EGADS originals GMA contains 27 edge groups GMA contains 14 face groups Wrote geometry-mesh associativity to caps.GeomToMesh.gma GeomToMesh I/O finished! Sat Jul 08 2023 10:49:33AM EDT Export Time: 00 Hours 00 Minutes 01 Seconds Volume mesh: Number of nodes = 7137 Number of elements = 41449 Number of triangles = 1262 Number of quadrilatarals = 0 Number of tetrahedrals = 41449 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Body = 1 Number of nodes = 635 Number of elements = 1262 Number of tris = 1262 Number of quad = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Writing global Glyph inputs... Writing egads file '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Sphere/caps.egads'.... Running pointwise...... Number of command line arguments = 2 Sat Jul 08 2023 10:49:35AM EDT Pointwise V18.5 Loading user defaults from capsUserDefaults.glf GeomToMesh: Defaults Connector level InitDim = 6 MaxDim = 8 MinDim = 3 TurnAngle = 0.000000 Deviation = 0.000000 SplitAngle = 0.000000 JoinCons = 0 ProxGrowthRate = 1.300000 SourceSpacing = 0 TurnAngleHard = 70.000000 EqualSpacing = 0 Domain level Algorithm = Delaunay FullLayers = 0 MaxLayers = 0 GrowthRate = 1.300000 IsoType = Triangle TRexType = Triangle TRexARLimit = 200.000000 TRexAngleBC = 0.000000 Decay = 0.500000 MinEdge = 0.000000 MaxEdge = 0.000000 Adapt = 0 WallSpacing = 0.000000 StrDomConvertARTrigger = 0.000000 Block level Algorithm = Delaunay VoxelLayers = 3 boundaryDecay = 0.500000 collisionBuffer = 0.500000 maxSkewAngle = 180.000000 TRexSkewDelay = 0 edgeMaxGrowthRate = 1.800000 fullLayers = 0 maxLayers = 0 growthRate = 1.300000 TRexType = TetPyramid volInitialize = 1 General SkipMeshing = 1 CAESolver = UGRID outerBoxScale = 0 sourceBoxLengthScale = 0.000000 sourceBoxDirection = 1.000000 0.000000 0.000000 sourceBoxAngle = 0.000000 sourceGrowthFactor = 10.000000 sourcePCDFile = ModelSize = 0 writeGMA = 2.0 assembleTolMult = 2.0 modelOrientIntMeshVolume = 1 Elevate On Export degree = Q1 costThreshold = 0.8 maxIncAngle = 175.0 relax = 0.05 smoothingPasses = 1000 WCNWeight = 0.5 WCNMode = Calculate writeVTU = false CADFile = caps.egads Determining model size from file. Info: Model Size adjusted to 10 Computing maximum DB edge tolerance. Quilt list has 8 entries. Quilt quilt-1: edge tolerance = 6.91474e-06 Quilt quilt-2: edge tolerance = 6.91474e-06 Quilt quilt-3: edge tolerance = 5e-08 Quilt quilt-4: edge tolerance = 5e-08 Quilt quilt-5: edge tolerance = 5e-08 Quilt quilt-6: edge tolerance = 5e-08 Quilt quilt-7: edge tolerance = 5e-08 Quilt quilt-8: edge tolerance = 5e-08 Maximum DB edge tolerance = 6.91474e-06 Performing model assembly pass on geometry entities. domParams(MinEdge) defined as 1.382948e-05 due to model assembly tolerance Looking for quilt names in geometry. Quilt list has 8 entries. Quilt list has 8 entries. Original connector list has 14 entries. Minimum connector length = 1.5708 Tolerance = 6.91474e-06 Performing merge on connectors with equal dimensions and common end points. After regular merge, connector list has 14 entries. Updating conData Min Edge Tol: 5.000e-08 on con-3 Max Edge Tol: 6.915e-06 on con-1 Adjusting connector dimensions based on average spacings. Checking dimension for connector 1/14, name = con-1 Checking dimension for connector 2/14, name = con-2 Checking dimension for connector 3/14, name = con-3 Changing dimension for connector 3/14 from 6 to 3 Checking dimension for connector 4/14, name = con-4 Changing dimension for connector 4/14 from 6 to 3 Checking dimension for connector 5/14, name = con-5 Changing dimension for connector 5/14 from 6 to 3 Checking dimension for connector 6/14, name = con-6 Changing dimension for connector 6/14 from 6 to 3 Checking dimension for connector 7/14, name = con-7 Changing dimension for connector 7/14 from 6 to 3 Checking dimension for connector 8/14, name = con-8 Changing dimension for connector 8/14 from 6 to 3 Checking dimension for connector 9/14, name = con-9 Changing dimension for connector 9/14 from 6 to 3 Checking dimension for connector 10/14, name = con-10 Changing dimension for connector 10/14 from 6 to 3 Checking dimension for connector 11/14, name = con-11 Checking dimension for connector 12/14, name = con-13 Checking dimension for connector 13/14, name = con-15 Checking dimension for connector 14/14, name = con-17 Processing spacing values for connector 1/14, name = con-1 Processing spacing values for connector 2/14, name = con-2 Processing spacing values for connector 3/14, name = con-3 Processing spacing values for connector 4/14, name = con-4 Processing spacing values for connector 5/14, name = con-5 Processing spacing values for connector 6/14, name = con-6 Processing spacing values for connector 7/14, name = con-7 Processing spacing values for connector 8/14, name = con-8 Processing spacing values for connector 9/14, name = con-9 Processing spacing values for connector 10/14, name = con-10 Processing spacing values for connector 11/14, name = con-11 Processing spacing values for connector 12/14, name = con-13 Processing spacing values for connector 13/14, name = con-15 Processing spacing values for connector 14/14, name = con-17 Number of unique endpoints = 10 Checking for baffle intersections. Performing Local Proximity Refinement Adjusting connector dimensions based on proximity to other connectors. Proximity test for connector 1/14, con-1. Proximity test for connector 2/14, con-2. Proximity test for connector 3/14, con-3. Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333 Proximity test for connector 4/14, con-4. Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333 Proximity test for connector 5/14, con-5. Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333 Proximity test for connector 6/14, con-6. Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333 Proximity test for connector 7/14, con-7. Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1 Proximity test for connector 8/14, con-8. Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1 Proximity test for connector 9/14, con-9. Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1 Proximity test for connector 10/14, con-10. Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1 Proximity test for connector 11/14, con-11. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 12/14, con-13. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 13/14, con-15. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Proximity test for connector 14/14, con-17. Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857 Adjusting node spacing from geometry Adjusting connector dimensions based on end spacings. Connector con-1 current dim = 6 Connector con-2 current dim = 6 Connector con-3 current dim = 4 Connector con-4 current dim = 4 Connector con-5 current dim = 4 Connector con-6 current dim = 4 Connector con-7 current dim = 5 Connector con-8 current dim = 5 Connector con-9 current dim = 5 Connector con-10 current dim = 5 Connector con-11 current dim = 8 Connector con-13 current dim = 8 Connector con-15 current dim = 8 Connector con-17 current dim = 8 Domain list has 8 entries. Looking for periodic domain attributes from geometry. Tolerance = 6.91474e-06 Number of periodic target domains = 0 Unstructured domain 1 of 8: boundary name = sphere. Creating boundary name sphere Unstructured domain 2 of 8: boundary name = sphere. sphere already in boundary name list. Unstructured domain 3 of 8: boundary name = farfield. Creating boundary name farfield Unstructured domain 4 of 8: boundary name = farfield. farfield already in boundary name list. Unstructured domain 5 of 8: boundary name = farfield. farfield already in boundary name list. Unstructured domain 6 of 8: boundary name = farfield. farfield already in boundary name list. Unstructured domain 7 of 8: boundary name = farfield. farfield already in boundary name list. Unstructured domain 8 of 8: boundary name = farfield. farfield already in boundary name list. Checking for blunt flag attribute on geometry faces. Performing initialization pass on all unstructured domains. Unstructured domain list for assembly has 8 entries. Structured domain list for assembly has 0 entries. Periodic target domain list for assembly has 0 entries. Creating unstructured block from 8 domains. Block = auto-blk Setting up unstructured block. Retrieving block attributes from geometry. Initializing unstructured block. CAE Solver set to UGRID GeomToMesh finished! Sat Jul 08 2023 10:49:36AM EDT Run Time: 00 Hours 00 Minutes 01 Seconds Pointwise save filename = caps.GeomToMesh.pw Sat Jul 08 2023 10:49:36AM EDT Exporting in UGRID format to file basename = caps.GeomToMesh Mapped 42 / 42 curves to EGADS originals GMA contains 14 edge groups GMA contains 8 face groups Wrote geometry-mesh associativity to caps.GeomToMesh.gma GeomToMesh I/O finished! Sat Jul 08 2023 10:49:37AM EDT Export Time: 00 Hours 00 Minutes 01 Seconds Volume mesh: Number of nodes = 603 Number of elements = 2992 Number of triangles = 354 Number of quadrilatarals = 0 Number of tetrahedrals = 2992 Number of pyramids = 0 Number of prisms = 0 Number of hexahedrals = 0 Body = 1 Number of nodes = 49 Number of elements = 94 Number of tris = 94 Number of quad = 0 Body = 2 Number of nodes = 132 Number of elements = 260 Number of tris = 260 Number of quad = 0 No project name ("Proj_Name") provided - A volume mesh will not be written out .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7766 Number of elements = 15528 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15528 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5870 Number of elements = 11736 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11736 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 488 Number of elements = 972 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14124 Total number of elements = 28236 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14124, elements - 28236 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.25217 Creating surface mesh ... Surface mesh seconds: 0.055945 Recovering boundaries... Boundary recovery seconds: 0.134036 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.085892 Recovering Delaunayness... Delaunay recovery seconds: 0.078286 Refining mesh... 18827 insertions, added 13420 points, 721721 tetrahedra in queue. 6269 insertions, added 2485 points, 625204 tetrahedra in queue. 8356 insertions, added 2101 points, 168215 tetrahedra in queue. Refinement seconds: 4.11755 Smoothing vertices... Mesh smoothing seconds: 3.29572 Improving mesh... Mesh improvement seconds: 0.187148 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.023295 Total running seconds: 8.23133 Statistics: Input points: 14124 Input facets: 28236 Input segments: 42354 Input holes: 2 Input regions: 0 Mesh points: 33059 Mesh tetrahedra: 159851 Mesh faces: 333820 Mesh faces on exterior boundary: 28236 Mesh faces on input facets: 28236 Mesh edges on input segments: 42354 Steiner points inside domain: 18935 Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Cardinal" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Raven" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Falcon" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " .Getting CFD boundary conditions Boundary condition name - Wing1 .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14124, elements - 28236 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2 1 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Running SU2 2 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14124, elements - 28236 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " CAPS Info: Hit last success -- going live! Running SU2 1 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " CAPS Info: Hit last success -- going live! Running SU2 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 15856, elements - 31700 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 1 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing boundary flags - bcProps.surfaceProp[0].surfaceType = 3 - bcProps.surfaceProp[1].surfaceType = 2 - bcProps.surfaceProp[2].surfaceType = 1 Done boundary flags Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "BlackBird (7.5.1) " .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - plate Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Getting FEA design variables....... Number of design variables - 2 Design_Variable name - plateLength Design_Variable name - thick1 Design_Variable_Relation name - thick1 Number of design variable relations - 1 Done getting FEA design variables Design_Constraint tuple is NULL - No design constraints applied Design_Equation tuple is NULL - No design equations applied Design_Table tuple is NULL - No design table constants applied Design_Opt_Param tuple is NULL - No design optimization parameters applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing TACS instruction file.... Writing analysis cards Writing load ADD cards Writing constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards FERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:58432) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 1 Name = box, index = 1 Getting surface mesh for body 1 (of 7) Getting surface mesh for body 2 (of 7) Getting surface mesh for body 3 (of 7) Getting surface mesh for body 4 (of 7) Getting surface mesh for body 5 (of 7) Getting surface mesh for body 6 (of 7) 7F05F2E51440 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7F05F2E51440 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7F05F2E51440 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7F05F2E51440 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 7) Body 1 (of 7) Number of nodes = 98 Number of elements = 192 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 192 Number of quadrilateral elements = 0 Body 2 (of 7) Number of nodes = 296 Number of elements = 588 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 588 Number of quadrilateral elements = 0 Body 3 (of 7) Number of nodes = 487 Number of elements = 970 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 970 Number of quadrilateral elements = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 4 (of 7) Number of nodes = 2048 Number of elements = 4096 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 7) Number of nodes = 152 Number of elements = 300 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 300 Number of quadrilateral elements = 0 Body 6 (of 7) Number of nodes = 624 Number of elements = 1248 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1248 Number of quadrilateral elements = 0 Body 7 (of 7) Number of nodes = 488 Number of elements = 972 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 972 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 4193 Total number of elements = 8366 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh for body 1 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.005247 Creating surface mesh ... Surface mesh seconds: 0.000684 Recovering boundaries... Boundary recovery seconds: 0.002285 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000191 Recovering Delaunayness... Delaunay recovery seconds: 0.001982 Refining mesh... Refinement seconds: 0.001463 Smoothing vertices... Mesh smoothing seconds: 0.005613 Improving mesh... Mesh improvement seconds: 0.000605 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000129 Total running seconds: 0.01831 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 0 Mesh points: 100 Mesh tetrahedra: 232 Mesh faces: 560 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 2 Done meshing using TetGen! Getting volume mesh for body 2 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cylinder, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.025756 Creating surface mesh ... Surface mesh seconds: 0.001758 Recovering boundaries... Boundary recovery seconds: 0.004987 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001212 Recovering Delaunayness... Delaunay recovery seconds: 0.007329 Refining mesh... Refinement seconds: 0.047538 Smoothing vertices... Mesh smoothing seconds: 0.043196 Improving mesh... Mesh improvement seconds: 0.002879 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000424 Total running seconds: 0.135239 Statistics: Input points: 296 Input facets: 588 Input segments: 882 Input holes: 0 Input regions: 0 Mesh points: 353 Mesh tetrahedra: 1100 Mesh faces: 2494 Mesh faces on exterior boundary: 588 Mesh faces on input facets: 588 Mesh edges on input segments: 882 Steiner points inside domain: 57 Done meshing using TetGen! Getting volume mesh for body 3 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = cone, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.106445 Creating surface mesh ... Surface mesh seconds: 0.003078 Recovering boundaries... Boundary recovery seconds: 0.012863 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.002752 Recovering Delaunayness... Delaunay recovery seconds: 0.026245 Refining mesh... 649 insertions, added 155 points, 7158 tetrahedra in queue. 216 insertions, added 12 points, 5981 tetrahedra in queue. 288 insertions, added 8 points, 2410 tetrahedra in queue. 383 insertions, added 17 points, 507 tetrahedra in queue. 511 insertions, added 13 points, 30 tetrahedra in queue. Refinement seconds: 0.333732 Smoothing vertices... Mesh smoothing seconds: 0.122956 Improving mesh... Mesh improvement seconds: 0.007453 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000844 Total running seconds: 0.616559 Statistics: Input points: 487 Input facets: 970 Input segments: 1455 Input holes: 0 Input regions: 0 Mesh points: 702 Mesh tetrahedra: 2858 Mesh faces: 6201 Mesh faces on exterior boundary: 970 Mesh faces on input facets: 970 Mesh edges on input segments: 1455 Steiner points inside domain: 215 Done meshing using TetGen! Getting volume mesh for body 4 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = torus, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.707346 Creating surface mesh ... Surface mesh seconds: 0.01287 Recovering boundaries... Boundary recovery seconds: 0.026549 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.012183 Recovering Delaunayness... Delaunay recovery seconds: 0.215939 Refining mesh... Refinement seconds: 0.654466 Smoothing vertices... Mesh smoothing seconds: 0.533055 Improving mesh... Mesh improvement seconds: 0.03187 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.003316 Total running seconds: 2.19812 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 0 Mesh points: 2914 Mesh tetrahedra: 11384 Mesh faces: 24816 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 866 Done meshing using TetGen! Getting volume mesh for body 5 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = sphere, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.001485 Creating surface mesh ... Surface mesh seconds: 0.001019 Recovering boundaries... Boundary recovery seconds: 0.001206 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000389 Recovering Delaunayness... Delaunay recovery seconds: 0.001396 Refining mesh... 202 insertions, added 45 points, 843 tetrahedra in queue. Refinement seconds: 0.018909 Smoothing vertices... Mesh smoothing seconds: 0.009922 Improving mesh... Mesh improvement seconds: 0.001218 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000199 Total running seconds: 0.035852 Statistics: Input points: 152 Input facets: 300 Input segments: 450 Input holes: 0 Input regions: 0 Mesh points: 199 Mesh tetrahedra: 677 Mesh faces: 1504 Mesh faces on exterior boundary: 300 Mesh faces on input facets: 300 Mesh edges on input segments: 450 Steiner points inside domain: 47 Done meshing using TetGen! Getting volume mesh for body 6 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = boxhole, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.079404 Creating surface mesh ... Surface mesh seconds: 0.00302 Recovering boundaries... Boundary recovery seconds: 0.009744 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.003432 Recovering Delaunayness... Delaunay recovery seconds: 0.013439 Refining mesh... 831 insertions, added 225 points, 6110 tetrahedra in queue. 276 insertions, added 14 points, 855 tetrahedra in queue. Refinement seconds: 0.163212 Smoothing vertices... Mesh smoothing seconds: 0.13082 Improving mesh... Mesh improvement seconds: 0.00868 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001001 Total running seconds: 0.413013 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 0 Mesh points: 863 Mesh tetrahedra: 3252 Mesh faces: 7128 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 239 Done meshing using TetGen! Getting volume mesh for body 7 (of 7) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = bullet, index = 1 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.073873 Creating surface mesh ... Surface mesh seconds: 0.002744 Recovering boundaries... Boundary recovery seconds: 0.013675 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.00188 Recovering Delaunayness... Delaunay recovery seconds: 0.06038 Refining mesh... Refinement seconds: 0.098838 Smoothing vertices... Mesh smoothing seconds: 0.074463 Improving mesh... Mesh improvement seconds: 0.006623 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000743 Total running seconds: 0.333474 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 0 Mesh points: 675 Mesh tetrahedra: 2506 Mesh faces: 5498 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 187 Done meshing using TetGen! Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Writing AFLR3 file .... Finished writing AFLR3 file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 7 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Body 1 number of surface: nodes - 98, elements - 192 Body 2 number of surface: nodes - 296, elements - 588 Body 3 number of surface: nodes - 487, elements - 970 Body 4 number of surface: nodes - 2048, elements - 4096 Body 5 number of surface: nodes - 152, elements - 300 Body 6 number of surface: nodes - 624, elements - 1248 Body 7 number of surface: nodes - 488, elements - 972 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.005122 Creating surface mesh ... Surface mesh seconds: 0.000531 Recovering boundaries... Boundary recovery seconds: 0.002103 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.000185 Recovering Delaunayness... Delaunay recovery seconds: 0.00189 Refining mesh... Refinement seconds: 0.001526 Smoothing vertices... Mesh smoothing seconds: 0.005567 Improving mesh... Mesh improvement seconds: 0.000598 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000166 Total running seconds: 0.017796 Statistics: Input points: 98 Input facets: 192 Input segments: 288 Input holes: 0 Input regions: 1 Mesh points: 100 Mesh tetrahedra: 232 Mesh faces: 560 Mesh faces on exterior boundary: 192 Mesh faces on input facets: 192 Mesh edges on input segments: 288 Steiner points inside domain: 2 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.025768 Creating surface mesh ... Surface mesh seconds: 0.001774 Recovering boundaries... Boundary recovery seconds: 0.00497 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001219 Recovering Delaunayness... Delaunay recovery seconds: 0.007091 Refining mesh... Refinement seconds: 0.046944 Smoothing vertices... Mesh smoothing seconds: 0.042208 Improving mesh... Mesh improvement seconds: 0.002839 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000441 Total running seconds: 0.133417 Statistics: Input points: 296 Input facets: 588 Input segments: 882 Input holes: 0 Input regions: 2 Mesh points: 353 Mesh tetrahedra: 1100 Mesh faces: 2494 Mesh faces on exterior boundary: 588 Mesh faces on input facets: 588 Mesh edges on input segments: 882 Steiner points inside domain: 57 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.105302 Creating surface mesh ... Surface mesh seconds: 0.00297 Recovering boundaries... Boundary recovery seconds: 0.012679 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.002718 Recovering Delaunayness... Delaunay recovery seconds: 0.026195 Refining mesh... 649 insertions, added 155 points, 7158 tetrahedra in queue. 216 insertions, added 12 points, 5981 tetrahedra in queue. 288 insertions, added 8 points, 2410 tetrahedra in queue. 383 insertions, added 17 points, 507 tetrahedra in queue. 511 insertions, added 13 points, 30 tetrahedra in queue. Refinement seconds: 0.327686 Smoothing vertices... Mesh smoothing seconds: 0.12048 Improving mesh... Mesh improvement seconds: 0.007299 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000801 Total running seconds: 0.606334 Statistics: Input points: 487 Input facets: 970 Input segments: 1455 Input holes: 0 Input regions: 3 Mesh points: 702 Mesh tetrahedra: 2858 Mesh faces: 6201 Mesh faces on exterior boundary: 970 Mesh faces on input facets: 970 Mesh edges on input segments: 1455 Steiner points inside domain: 215 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.69728 Creating surface mesh ... Surface mesh seconds: 0.01213 Recovering boundaries... Boundary recovery seconds: 0.024959 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.010982 Recovering Delaunayness... Delaunay recovery seconds: 0.213611 Refining mesh... Refinement seconds: 0.645455 Smoothing vertices... Mesh smoothing seconds: 0.513399 Improving mesh... Mesh improvement seconds: 0.031373 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00319 Total running seconds: 2.1529 Statistics: Input points: 2048 Input facets: 4096 Input segments: 6144 Input holes: 0 Input regions: 4 Mesh points: 2893 Mesh tetrahedra: 11251 Mesh faces: 24550 Mesh faces on exterior boundary: 4096 Mesh faces on input facets: 4096 Mesh edges on input segments: 6144 Steiner points inside domain: 845 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.001646 Creating surface mesh ... Surface mesh seconds: 0.000941 Recovering boundaries... Boundary recovery seconds: 0.001139 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.000463 Recovering Delaunayness... Delaunay recovery seconds: 0.001259 Refining mesh... 202 insertions, added 45 points, 843 tetrahedra in queue. Refinement seconds: 0.018359 Smoothing vertices... Mesh smoothing seconds: 0.0127 Improving mesh... Mesh improvement seconds: 0.00151 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000257 Total running seconds: 0.038395 Statistics: Input points: 152 Input facets: 300 Input segments: 450 Input holes: 0 Input regions: 5 Mesh points: 199 Mesh tetrahedra: 677 Mesh faces: 1504 Mesh faces on exterior boundary: 300 Mesh faces on input facets: 300 Mesh edges on input segments: 450 Steiner points inside domain: 47 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.086739 Creating surface mesh ... Surface mesh seconds: 0.003569 Recovering boundaries... Boundary recovery seconds: 0.010261 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.003136 Recovering Delaunayness... Delaunay recovery seconds: 0.01254 Refining mesh... 831 insertions, added 225 points, 6110 tetrahedra in queue. 276 insertions, added 14 points, 855 tetrahedra in queue. Refinement seconds: 0.159721 Smoothing vertices... Mesh smoothing seconds: 0.128053 Improving mesh... Mesh improvement seconds: 0.008521 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000962 Total running seconds: 0.413722 Statistics: Input points: 624 Input facets: 1248 Input segments: 1872 Input holes: 0 Input regions: 6 Mesh points: 863 Mesh tetrahedra: 3252 Mesh faces: 7128 Mesh faces on exterior boundary: 1248 Mesh faces on input facets: 1248 Mesh edges on input segments: 1872 Steiner points inside domain: 239 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.073273 Creating surface mesh ... Surface mesh seconds: 0.002923 Recovering boundaries... Boundary recovery seconds: 0.013615 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Warning: The 2-th region point lies outside the convex hull. Warning: The 3-th region point lies outside the convex hull. Warning: The 4-th region point lies outside the convex hull. Warning: The 5-th region point lies outside the convex hull. Warning: The 6-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001958 Recovering Delaunayness... Delaunay recovery seconds: 0.061159 Refining mesh... Refinement seconds: 0.100584 Smoothing vertices... Mesh smoothing seconds: 0.080248 Improving mesh... Mesh improvement seconds: 0.006713 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000713 Total running seconds: 0.341397 Statistics: Input points: 488 Input facets: 972 Input segments: 1458 Input holes: 0 Input regions: 7 Mesh points: 674 Mesh tetrahedra: 2508 Mesh faces: 5502 Mesh faces on exterior boundary: 972 Mesh faces on input facets: 972 Mesh edges on input segments: 1458 Steiner points inside domain: 186 Done meshing using TetGen! Writing AFLR3 file .... Finished writing AFLR3 file .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 CAPS Info: Hit last success -- going live! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! CAPS Info: Hit last success -- going live! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 7130, elements - 14252 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Farfield, index = 1 Name = Wing1, index = 2 Name = trailingEdge, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9626 Number of elements = 19244 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19244 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9626 Total number of elements = 19244 Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000QT1.00e-16A Done meshing using TetGen! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Number of surface: nodes - 9626, elements - 19244 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq2.000/0.000QT1.00e-16A Done meshing using TetGen! Writing TECPLOT file: test.dat .... Finished writing TECPLOT file . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! ......... ====================================================================== ERROR: test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D) ---------------------------------------------------------------------- Traceback (most recent call last): File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/test_fun3d.py", line 427, in test_Mesh_Morph_Sensitivity self.fun3d.preAnalysis() File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 2140, in preAnalysis self._analysisObj.preAnalysis() File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 2861, in preAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: EGADS_NULLOBJ: ================================================================================ aimMesh.c:1542 in aim_morphMeshUpdate(): Error status = -2 fun3dAIM.c:1069 in aimUpdateState(): Error status = -2 ================================================================================ ====================================================================== FAIL: test_PlateSensFile (test_tacs.TestTACS) ---------------------------------------------------------------------- Traceback (most recent call last): File "/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/test_tacs.py", line 163, in test_PlateSensFile self.assertAlmostEqual(Func1_plateLength, xyz[inode][0], 5) AssertionError: 0.0 != 0.5 within 5 places (0.5 difference) ---------------------------------------------------------------------- Ran 123 tests in 2120.837s FAILED (failures=1, errors=1, skipped=2) CAPS Error: Cannot open /jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS/workDir_fun3dTest/Scratch/capsRestart/Problem! CAPS Warning: caps_writeProblem = -333 (caps_close)! make[1]: *** [Makefile:4: test] Error 1 make[1]: Leaving directory '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64/CAPS/aim/unitTest/pyCAPS' make: *** [Makefile:75: unitaim] Error 2 ++ true [GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/LINUX64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.6,CAPS/unit,LINUX64,reynolds) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/unit,ESP_ARCH=LINUX64,buildnode=reynolds #183' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [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_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/unit,ESP_ARCH=LINUX64,buildnode=reynolds #184'. [Checks API] No suitable checks publisher found. Build step 'Console output (build log) parsing' changed build result to FAILURE [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] Skipped based on build state FAILURE Finished: FAILURE