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Skipping 776 KB.. Full LogTetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.185089 Creating surface mesh ... Surface mesh seconds: 0.00191 Recovering boundaries... Boundary recovery seconds: 0.00999 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: 0.000818 Recovering Delaunayness... Delaunay recovery seconds: 0.05497 Refining mesh... Refinement seconds: 0.134558 Smoothing vertices... Mesh smoothing seconds: 0.125636 Improving mesh... Mesh improvement seconds: 0.002377 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.000437 Total running seconds: 0.515857 Statistics: Input points: 1070 Input facets: 2136 Input segments: 3204 Input holes: 0 Input regions: 5 Mesh points: 1321 Mesh tetrahedra: 4502 Mesh faces: 10072 Mesh faces on exterior boundary: 2136 Mesh faces on input facets: 2136 Mesh edges on input segments: 3204 Steiner points inside domain: 251 Done meshing using TetGen! Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing exodus file .... Block: 'tableTop_tet', blk_id 1, num_entries 1722 Block: 'leg0_tet', blk_id 2, num_entries 4467 Block: 'leg1_tet', blk_id 3, num_entries 4468 Block: 'leg2_tet', blk_id 4, num_entries 4517 Block: 'leg3_tet', blk_id 5, num_entries 4502 Sideset: 'leg0Side', set_id 1, num_entries 2136 Sideset: 'leg1Side', set_id 2, num_entries 2136 Sideset: 'leg2Side', set_id 3, num_entries 2136 Sideset: 'leg3Side', set_id 4, num_entries 2136 Sideset: 'tableTopSide', set_id 5, num_entries 1280 Nodeset: 'edge', set_id 1, num_entries 17 Nodeset: 'face1', set_id 2, num_entries 99 Nodeset: 'face2', set_id 3, num_entries 99 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file real 0m4.327s user 0m3.670s sys 0m0.265s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_tetgen_table_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_tetgen_cyli_box_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt plato_tetgen_cyli_box_PyTest.py test; + python -u plato_tetgen_cyli_box_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt EGADS Warning: Loop 2 marked with -1 EGADS Warning: Loop 2 marked with -1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 3591 Number of elements = 7306 Number of triangle elements = 7306 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 3591 Total number of elements = 7306 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Number of surface: nodes - 3591, elements - 7306 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.371042 Creating surface mesh ... Surface mesh seconds: 0.004788 Recovering boundaries... Boundary recovery seconds: 0.044699 Removing exterior tetrahedra ... Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.001318 Recovering Delaunayness... Delaunay recovery seconds: 0.271558 Refining mesh... Refinement seconds: 0.484043 Smoothing vertices... Mesh smoothing seconds: 0.570139 Improving mesh... Mesh improvement seconds: 0.007062 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002731 Total running seconds: 1.75753 Statistics: Input points: 3591 Input facets: 7306 Input segments: 10895 Input holes: 0 Input regions: 3 Mesh points: 5613 Mesh tetrahedra: 29362 Mesh faces: 60329 Mesh faces on exterior boundary: 3210 Mesh faces on input facets: 7306 Mesh edges on input segments: 10895 Steiner points inside domain: 2022 Done meshing using TetGen! Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing exodus file .... Block: 'c_tet', blk_id 1, num_entries 12754 Block: 'b_tet', blk_id 2, num_entries 11091 Block: 'a_tet', blk_id 3, num_entries 5517 Sideset: 'box', set_id 1, num_entries 3210 Sideset: 'cyl1', set_id 2, num_entries 2116 Sideset: 'cyl2', set_id 3, num_entries 2310 Finished writing Exodus file real 0m3.615s user 0m3.191s sys 0m0.235s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_tetgen_cyli_box_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_aflr_tetgen_table_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt plato_aflr_tetgen_table_PyTest.py test; + python -u plato_aflr_tetgen_table_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 5 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 4 Faces EGADS : Body 1 has 6 Edges EGADS : Body 1 has 4 Loops EGADS : Body 1 has 4 Nodes EGADS : Body 2 is a SolidBody EGADS : Body 2 has 1 Shells EGADS : Body 2 has 4 Faces EGADS : Body 2 has 6 Edges EGADS : Body 2 has 4 Loops EGADS : Body 2 has 4 Nodes EGADS : Body 3 is a SolidBody EGADS : Body 3 has 1 Shells EGADS : Body 3 has 4 Faces EGADS : Body 3 has 6 Edges EGADS : Body 3 has 4 Loops EGADS : Body 3 has 4 Nodes EGADS : Body 4 is a SolidBody EGADS : Body 4 has 1 Shells EGADS : Body 4 has 4 Faces EGADS : Body 4 has 6 Edges EGADS : Body 4 has 4 Loops EGADS : Body 4 has 4 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 0 1 8 9 10 EGADS : 8 Yes 1 0 1 0 1 7 9 10 EGADS : 9 Yes 1 0 1 0 1 7 8 EGADS : 10 Yes 1 0 1 0 1 7 8 EGADS : 11 Yes 2 0 1 0 1 12 13 14 EGADS : 12 Yes 2 0 1 0 1 11 13 14 EGADS : 13 Yes 2 0 1 0 1 11 12 EGADS : 14 Yes 2 0 1 0 1 11 12 EGADS : 15 Yes 3 0 1 0 1 16 17 18 EGADS : 16 Yes 3 0 1 0 1 15 17 18 EGADS : 17 Yes 3 0 1 0 1 15 16 EGADS : 18 Yes 3 0 1 0 1 15 16 EGADS : 19 Yes 4 0 1 0 1 20 21 22 EGADS : 20 Yes 4 0 1 0 1 19 21 22 EGADS : 21 Yes 4 0 1 0 1 19 20 EGADS : 22 Yes 4 0 1 0 1 19 20 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 -13 -14 15 16 EGADS : 8 17 14 -18 -16 EGADS : 9 13 18 EGADS : 10 -15 -17 EGADS : 11 -19 -20 21 22 EGADS : 12 23 20 -24 -22 EGADS : 13 19 24 EGADS : 14 -21 -23 EGADS : 15 -25 -26 27 28 EGADS : 16 29 26 -30 -28 EGADS : 17 25 30 EGADS : 18 -27 -29 EGADS : 19 -31 -32 33 34 EGADS : 20 35 32 -36 -34 EGADS : 21 31 36 EGADS : 22 -33 -35 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : 15 15 EGADS : 16 16 EGADS : 17 17 EGADS : 18 18 EGADS : 19 19 EGADS : 20 20 EGADS : 21 21 EGADS : 22 22 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes -5 8 7 -6 EGADS : 3 Yes 9 5 -10 -1 EGADS : 4 Yes -11 3 12 -7 EGADS : 5 Yes 4 11 -8 -9 EGADS : 6 Yes -2 10 6 -12 EGADS : 7 Yes -13 -14 15 16 EGADS : 8 Yes 17 14 -18 -16 EGADS : 9 Yes 13 18 EGADS : 10 Yes -15 -17 EGADS : 11 Yes -19 -20 21 22 EGADS : 12 Yes 23 20 -24 -22 EGADS : 13 Yes 19 24 EGADS : 14 Yes -21 -23 EGADS : 15 Yes -25 -26 27 28 EGADS : 16 Yes 29 26 -30 -28 EGADS : 17 Yes 25 30 EGADS : 18 Yes -27 -29 EGADS : 19 Yes -31 -32 33 34 EGADS : 20 Yes 35 32 -36 -34 EGADS : 21 Yes 31 36 EGADS : 22 Yes -33 -35 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 10 9 1 7 9 EGADS : 14 1 Yes 11 10 1 7 8 EGADS : 15 1 Yes 11 12 1 7 10 EGADS : 16 1 Yes 12 9 1 7 8 EGADS : 17 1 Yes 12 11 1 8 10 EGADS : 18 1 Yes 9 10 1 8 9 EGADS : 19 2 Yes 14 13 1 11 13 EGADS : 20 2 Yes 15 14 1 11 12 EGADS : 21 2 Yes 15 16 1 11 14 EGADS : 22 2 Yes 16 13 1 11 12 EGADS : 23 2 Yes 16 15 1 12 14 EGADS : 24 2 Yes 13 14 1 12 13 EGADS : 25 3 Yes 18 17 1 15 17 EGADS : 26 3 Yes 19 18 1 15 16 EGADS : 27 3 Yes 19 20 1 15 18 EGADS : 28 3 Yes 20 17 1 15 16 EGADS : 29 3 Yes 20 19 1 16 18 EGADS : 30 3 Yes 17 18 1 16 17 EGADS : 31 4 Yes 22 21 1 19 21 EGADS : 32 4 Yes 23 22 1 19 20 EGADS : 33 4 Yes 23 24 1 19 22 EGADS : 34 4 Yes 24 21 1 19 20 EGADS : 35 4 Yes 24 23 1 20 22 EGADS : 36 4 Yes 21 22 1 20 21 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.1 0.5 EGADS : 4 Yes 0 0.1 0 EGADS : 5 Yes 0.5 0 0.5 EGADS : 6 Yes 0.5 0 0 EGADS : 7 Yes 0.5 0.1 0.5 EGADS : 8 Yes 0.5 0.1 0 EGADS : 9 Yes 0 0 0 EGADS : 10 Yes 0 0 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 0 0 0 EGADS : 13 Yes 0 0 0.26 EGADS : 14 Yes 0 0 0.46 EGADS : 15 Yes 0 0 0.46 EGADS : 16 Yes 0 0 0.26 EGADS : 17 Yes 0.36 0 0.26 EGADS : 18 Yes 0.36 0 0.46 EGADS : 19 Yes 0.36 0 0.46 EGADS : 20 Yes 0.36 0 0.26 EGADS : 21 Yes 0.36 0 0 EGADS : 22 Yes 0.36 0 0 EGADS : 23 Yes 0.36 0 0 EGADS : 24 Yes 0.36 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 1 AFLR4 : Min Bounding Box Length = 0.7 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 0.7 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.005 AFLR4 : Max Surf Spacing = 0.1 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : 15 CAD geometry 0 STD w/BL AFLR4 : 16 CAD geometry 0 STD w/BL AFLR4 : 17 CAD geometry 0 STD w/BL AFLR4 : 18 CAD geometry 0 STD w/BL AFLR4 : 19 CAD geometry 0 STD w/BL AFLR4 : 20 CAD geometry 0 STD w/BL AFLR4 : 21 CAD geometry 0 STD w/BL AFLR4 : 22 CAD geometry 0 STD w/BL AFLR4 : Case has 5 Proximity Checking Components AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 AFLR4 : Component 2 includes Definitions 7 8 9 10 AFLR4 : Component 3 includes Definitions 11 12 13 14 AFLR4 : Component 4 includes Definitions 15 16 17 18 AFLR4 : Component 5 includes Definitions 19 20 21 22 AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Define CAD surface definition 15 AFLR4 : Define CAD surface definition 16 AFLR4 : Define CAD surface definition 17 AFLR4 : Define CAD surface definition 18 AFLR4 : Define CAD surface definition 19 AFLR4 : Define CAD surface definition 20 AFLR4 : Define CAD surface definition 21 AFLR4 : Define CAD surface definition 22 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 229 400 0 AFLR4 : Nodes, Trias,Quads= 212 366 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 230 402 0 AFLR4 : Nodes, Trias,Quads= 212 366 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 49 64 0 AFLR4 : Nodes, Trias,Quads= 34 34 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2258 4330 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2270 4354 0 AFLR4 : Nodes, Trias,Quads= 2259 4332 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 20764 41508 2224 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 20764 41508 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 201 348 0 AFLR4 : Nodes, Trias,Quads= 193 332 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 204 354 0 AFLR4 : Nodes, Trias,Quads= 193 332 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 46 60 0 AFLR4 : Nodes, Trias,Quads= 30 28 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2244 4302 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2250 4314 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2244 4302 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2250 4314 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2245 4304 0 AFLR4 : Nodes, Trias,Quads= 2243 4300 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Nodes, Trias,Quads= 2248 4310 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 496 926 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 502 938 0 AFLR4 : Nodes, Trias,Quads= 408 750 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 20655 41290 2208 AFLR4 : Proximity BG Surface Grid Generation AFLR4 : Nodes, Trias = 21568 43116 AFLR4 : Nodes, Trias = 22452 44884 AFLR4 : Nodes, Trias = 22544 45068 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 311 517 0 AFLR4 : Nodes, Trias,Quads= 309 513 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 313 521 0 AFLR4 : Nodes, Trias,Quads= 309 513 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 3277 6339 0 AFLR4 : Nodes, Trias,Quads= 1431 2647 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1864 3566 0 AFLR4 : Nodes, Trias,Quads= 1736 3310 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 315 525 0 AFLR4 : Nodes, Trias,Quads= 307 509 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 318 530 0 AFLR4 : Nodes, Trias,Quads= 314 522 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2271 4352 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2276 4362 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2273 4356 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2277 4364 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 2301 4412 0 AFLR4 : Nodes, Trias,Quads= 2272 4354 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 2302 4414 0 AFLR4 : Nodes, Trias,Quads= 2273 4356 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 548 1028 0 AFLR4 : Nodes, Trias,Quads= 423 778 0 AFLR4 : Generate optimal mesh on surface definition 22 AFLR2 : Nodes, Trias,Quads= 549 1030 0 AFLR4 : Nodes, Trias,Quads= 418 768 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 24535 49050 2818 OVERALL : CPU Time = 1.436 seconds Body 1 (of 5) Number of nodes = 4009 Number of elements = 8014 Number of triangle elements = 8014 Number of quadrilateral elements = 0 Body 2 (of 5) Number of nodes = 5132 Number of elements = 10260 Number of triangle elements = 10260 Number of quadrilateral elements = 0 Body 3 (of 5) Number of nodes = 5130 Number of elements = 10256 Number of triangle elements = 10256 Number of quadrilateral elements = 0 Body 4 (of 5) Number of nodes = 5134 Number of elements = 10264 Number of triangle elements = 10264 Number of quadrilateral elements = 0 Body 5 (of 5) Number of nodes = 5130 Number of elements = 10256 Number of triangle elements = 10256 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 24535 Total number of elements = 49050 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = tableTopSide, index = 1 Name = leg0Side, index = 2 Name = leg1Side, index = 3 Name = leg2Side, index = 4 Name = leg3Side, index = 5 Body 1 number of surface: nodes - 4009, elements - 8014 Body 2 number of surface: nodes - 5132, elements - 10260 Body 3 number of surface: nodes - 5130, elements - 10256 Body 4 number of surface: nodes - 5134, elements - 10264 Body 5 number of surface: nodes - 5130, elements - 10256 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.043001 Creating surface mesh ... Surface mesh seconds: 0.005827 Recovering boundaries... Boundary recovery seconds: 0.021664 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.001267 Recovering Delaunayness... Delaunay recovery seconds: 0.0041 Refining mesh... Refinement seconds: 0.039324 Smoothing vertices... Mesh smoothing seconds: 0.060411 Improving mesh... Mesh improvement seconds: 0.003216 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.002699 Total running seconds: 0.181627 Statistics: Input points: 4009 Input facets: 8014 Input segments: 12021 Input holes: 0 Input regions: 1 Mesh points: 4748 Mesh tetrahedra: 15739 Mesh faces: 35485 Mesh faces on exterior boundary: 8014 Mesh faces on input facets: 8014 Mesh edges on input segments: 12021 Steiner points inside domain: 739 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.064746 Creating surface mesh ... Surface mesh seconds: 0.006646 Recovering boundaries... Boundary recovery seconds: 0.052362 Removing exterior tetrahedra ... Warning: The 1-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.01697 Recovering Delaunayness... Delaunay recovery seconds: 0.016884 Refining mesh... Refinement seconds: 0.133341 Smoothing vertices... Mesh smoothing seconds: 0.116013 Improving mesh... Mesh improvement seconds: 0.004974 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001291 Total running seconds: 0.413392 Statistics: Input points: 5132 Input facets: 10260 Input segments: 15390 Input holes: 0 Input regions: 2 Mesh points: 6604 Mesh tetrahedra: 23362 Mesh faces: 51854 Mesh faces on exterior boundary: 10260 Mesh faces on input facets: 10260 Mesh edges on input segments: 15390 Steiner points inside domain: 1472 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.06282 Creating surface mesh ... Surface mesh seconds: 0.003818 Recovering boundaries... Boundary recovery seconds: 0.037881 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: 0.01778 Recovering Delaunayness... Delaunay recovery seconds: 0.015661 Refining mesh... Refinement seconds: 0.094651 Smoothing vertices... Mesh smoothing seconds: 0.10632 Improving mesh... Mesh improvement seconds: 0.006764 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.001122 Total running seconds: 0.347039 Statistics: Input points: 5130 Input facets: 10256 Input segments: 15384 Input holes: 0 Input regions: 3 Mesh points: 6596 Mesh tetrahedra: 23355 Mesh faces: 51838 Mesh faces on exterior boundary: 10256 Mesh faces on input facets: 10256 Mesh edges on input segments: 15384 Steiner points inside domain: 1466 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.066081 Creating surface mesh ... Surface mesh seconds: 0.003485 Recovering boundaries... Boundary recovery seconds: 0.057863 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: 0.026373 Recovering Delaunayness... Delaunay recovery seconds: 0.018966 Refining mesh... Refinement seconds: 0.146303 Smoothing vertices... Mesh smoothing seconds: 0.148481 Improving mesh... Mesh improvement seconds: 0.007725 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.00357 Total running seconds: 0.479001 Statistics: Input points: 5134 Input facets: 10264 Input segments: 15396 Input holes: 0 Input regions: 4 Mesh points: 6618 Mesh tetrahedra: 23443 Mesh faces: 52018 Mesh faces on exterior boundary: 10264 Mesh faces on input facets: 10264 Mesh edges on input segments: 15396 Steiner points inside domain: 1484 Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.065788 Creating surface mesh ... Surface mesh seconds: 0.003768 Recovering boundaries... Boundary recovery seconds: 0.057413 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: 0.022837 Recovering Delaunayness... Delaunay recovery seconds: 0.014011 Refining mesh... Refinement seconds: 0.150132 Smoothing vertices... Mesh smoothing seconds: 0.151226 Improving mesh... Mesh improvement seconds: 0.008998 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.0011 Total running seconds: 0.475433 Statistics: Input points: 5130 Input facets: 10256 Input segments: 15384 Input holes: 0 Input regions: 5 Mesh points: 6595 Mesh tetrahedra: 23365 Mesh faces: 51858 Mesh faces on exterior boundary: 10256 Mesh faces on input facets: 10256 Mesh edges on input segments: 15384 Steiner points inside domain: 1465 Done meshing using TetGen! Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing exodus file .... Block: 'tableTop_tet', blk_id 1, num_entries 15739 Block: 'leg0_tet', blk_id 2, num_entries 23362 Block: 'leg1_tet', blk_id 3, num_entries 23355 Block: 'leg2_tet', blk_id 4, num_entries 23443 Block: 'leg3_tet', blk_id 5, num_entries 23365 Sideset: 'leg0Side', set_id 1, num_entries 10260 Sideset: 'leg1Side', set_id 2, num_entries 10256 Sideset: 'leg2Side', set_id 3, num_entries 10264 Sideset: 'leg3Side', set_id 4, num_entries 10256 Sideset: 'tableTopSide', set_id 5, num_entries 8014 Nodeset: 'edge', set_id 1, num_entries 41 Nodeset: 'face1', set_id 2, num_entries 610 Nodeset: 'face2', set_id 3, num_entries 617 Nodeset: 'node', set_id 4, num_entries 1 Finished writing Exodus file real 0m7.951s user 0m4.992s sys 0m0.311s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_aflr_tetgen_table_PyTest.py passed (as expected) ================================================= ================================================= + echo 'plato_aflr_tetgen_cyli_box_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt plato_aflr_tetgen_cyli_box_PyTest.py test; + python -u plato_aflr_tetgen_cyli_box_PyTest.py -outLevel=0 + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/pyCAPSlog.txt EGADS Warning: Loop 2 marked with -1 EGADS Warning: Loop 2 marked with -1 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 AFLR2 : --------------------------------------- AFLR2 : AFLR2 LIBRARY AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR2 : TRIA/QUAD GRID GENERATOR AFLR2 : Version Number 9.17.15 AFLR2 : Version Date 04/23/24 @ 12:51AM AFLR2 : Compile OS Darwin 23.4.0 arm64 AFLR2 : Compile Date 04/23/24 @ 12:51AM AFLR2 : Copyright 1994-2021, D.L. Marcum AFLR2 : --------------------------------------- AFLR4 : --------------------------------------- AFLR4 : AFLR4 LIBRARY AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR AFLR4 : Version Number 11.5.14 AFLR4 : Version Date 04/18/24 @ 12:45PM AFLR4 : Compile OS Darwin 23.4.0 arm64 AFLR4 : Compile Date 04/18/24 @ 03:04PM AFLR4 : Copyright 1994-2021, D.L. Marcum AFLR4 : --------------------------------------- EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.7.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SheetBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 24 Edges EGADS : Body 0 has 18 Loops EGADS : Body 0 has 16 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 6 7 8 EGADS : 2 Yes 0 0 1 0 1 1 3 4 5 7 8 9 EGADS : 3 Yes 0 0 1 0 1 2 4 6 9 12 EGADS : 4 Yes 0 0 1 0 1 2 3 6 9 12 EGADS : 5 Yes 0 0 1 0 1 2 6 7 8 EGADS : 6 Yes 0 0 1 0 1 1 3 4 5 7 8 12 EGADS : 7 Yes 0 0 1 0 1 1 2 5 6 EGADS : 8 Yes 0 0 1 0 1 1 2 5 6 EGADS : 9 Yes 0 0 1 0 1 2 3 4 10 11 13 EGADS : 10 Yes 0 0 1 0 1 9 11 12 13 14 EGADS : 11 Yes 0 0 1 0 1 9 10 12 13 14 EGADS : 12 Yes 0 0 1 0 1 3 4 6 10 11 14 EGADS : 13 Yes 0 0 1 0 1 9 10 11 EGADS : 14 Yes 0 0 1 0 1 10 11 12 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 4 3 -2 EGADS : 2 5 1 -6 -7 8 9 EGADS : 3 10 -12 -11 8 EGADS : 4 -10 9 11 -13 EGADS : 5 7 14 -15 -16 EGADS : 6 -17 15 18 -3 -12 -13 EGADS : 7 16 17 -4 -5 EGADS : 8 -14 6 2 -18 EGADS : 9 -8 -9 19 20 EGADS : 10 21 -23 -22 19 EGADS : 11 -21 20 22 -24 EGADS : 12 12 13 -23 -24 EGADS : 13 -19 -20 EGADS : 14 23 24 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 3 EGADS : 3 4 EGADS : 4 5 EGADS : 5 6 EGADS : 6 7 8 EGADS : 7 9 EGADS : 8 10 EGADS : 9 11 12 EGADS : 10 13 EGADS : 11 14 EGADS : 12 15 16 EGADS : 13 17 EGADS : 14 18 EGADS : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 4 3 -2 EGADS : 2 Yes 5 1 -6 -7 EGADS : 3 Yes 8 9 EGADS : 4 Yes 10 -12 -11 8 EGADS : 5 Yes -10 9 11 -13 EGADS : 6 Yes 7 14 -15 -16 EGADS : 7 Yes -17 15 18 -3 EGADS : 8 Yes -12 -13 EGADS : 9 Yes 16 17 -4 -5 EGADS : 10 Yes -14 6 2 -18 EGADS : 11 Yes -8 -9 EGADS : 12 Yes 19 20 EGADS : 13 Yes 21 -23 -22 19 EGADS : 14 Yes -21 20 22 -24 EGADS : 15 Yes 12 13 EGADS : 16 Yes -23 -24 EGADS : 17 Yes -19 -20 EGADS : 18 Yes 23 24 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 2 EGADS : 2 0 Yes 1 3 1 1 8 EGADS : 3 0 Yes 4 3 1 1 6 EGADS : 4 0 Yes 2 4 1 1 7 EGADS : 5 0 Yes 5 2 1 2 7 EGADS : 6 0 Yes 6 1 1 2 8 EGADS : 7 0 Yes 5 6 1 2 5 EGADS : 8 0 Yes 7 8 1 2 3 9 EGADS : 9 0 Yes 8 7 1 2 4 9 EGADS : 10 0 Yes 8 9 1 3 4 EGADS : 11 0 Yes 7 10 1 3 4 EGADS : 12 0 Yes 10 9 1 3 6 12 EGADS : 13 0 Yes 9 10 1 4 6 12 EGADS : 14 0 Yes 6 11 1 5 8 EGADS : 15 0 Yes 12 11 1 5 6 EGADS : 16 0 Yes 5 12 1 5 7 EGADS : 17 0 Yes 12 4 1 6 7 EGADS : 18 0 Yes 11 3 1 6 8 EGADS : 19 0 Yes 13 14 1 9 10 13 EGADS : 20 0 Yes 14 13 1 9 11 13 EGADS : 21 0 Yes 14 15 1 10 11 EGADS : 22 0 Yes 13 16 1 10 11 EGADS : 23 0 Yes 16 15 1 10 12 14 EGADS : 24 0 Yes 15 16 1 11 12 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0.5 0 0.5 EGADS : 2 Yes 0.5 0 0 EGADS : 3 Yes 0.5 0.5 0.5 EGADS : 4 Yes 0.5 0.5 0 EGADS : 5 Yes 0 0 0 EGADS : 6 Yes 0 0 0.5 EGADS : 7 Yes 0 0 0.2 EGADS : 8 Yes 0 0 0 EGADS : 9 Yes 0 0.5 0 EGADS : 10 Yes 0 0.5 0.2 EGADS : 11 Yes 0 0.5 0.5 EGADS : 12 Yes 0 0.5 0 EGADS : 13 Yes 0 0 0.1 EGADS : 14 Yes 0 0 0 EGADS : 15 Yes 0 0.5 0 EGADS : 16 Yes 0 0.5 0.1 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 1 AFLR4 : Min Bounding Box Length = 1 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.005 AFLR4 : Max Surf Spacing = 0.1 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD AFLR4 : 2 CAD geometry 0 STD AFLR4 : 3 CAD geometry 0 TRANSP AFLR4 : 4 CAD geometry 0 TRANSP AFLR4 : 5 CAD geometry 0 STD AFLR4 : 6 CAD geometry 0 STD AFLR4 : 7 CAD geometry 0 STD AFLR4 : 8 CAD geometry 0 STD AFLR4 : 9 CAD geometry 0 STD AFLR4 : 10 CAD geometry 0 TRANSP AFLR4 : 11 CAD geometry 0 TRANSP AFLR4 : 12 CAD geometry 0 STD AFLR4 : 13 CAD geometry 0 STD AFLR4 : 14 CAD geometry 0 STD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 486 868 0 AFLR4 : Nodes, Trias,Quads= 477 850 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1904 3642 0 AFLR4 : Nodes, Trias,Quads= 1889 3612 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1904 3642 0 AFLR4 : Nodes, Trias,Quads= 1889 3612 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 486 868 0 AFLR4 : Nodes, Trias,Quads= 476 848 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 582 1036 0 AFLR4 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 3745 7224 0 AFLR4 : Nodes, Trias,Quads= 3741 7216 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 3745 7224 0 AFLR4 : Nodes, Trias,Quads= 3741 7216 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 582 1036 0 AFLR4 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 402 738 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 515 964 0 AFLR4 : Nodes, Trias,Quads= 413 760 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 13768 27788 1608 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 13768 27788 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 507 910 0 AFLR4 : Nodes, Trias,Quads= 713 1322 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 1877 3588 0 AFLR4 : Nodes, Trias,Quads= 1884 3602 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 1876 3586 0 AFLR4 : Nodes, Trias,Quads= 1883 3600 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 507 910 0 AFLR4 : Nodes, Trias,Quads= 710 1316 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 3736 7206 0 AFLR4 : Nodes, Trias,Quads= 3727 7188 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 3735 7204 0 AFLR4 : Nodes, Trias,Quads= 3731 7196 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Nodes, Trias,Quads= 576 1024 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 504 942 0 AFLR4 : Nodes, Trias,Quads= 406 746 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 498 930 0 AFLR4 : Nodes, Trias,Quads= 416 766 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 14210 28672 1608 OVERALL : CPU Time = 0.346 seconds Body 1 (of 1) Number of nodes = 14210 Number of elements = 28672 Number of triangle elements = 28672 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14210 Total number of elements = 28672 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = box, index = 1 Name = cyl2, index = 2 Name = box;cyl2, index = 3 Name = cyl1, index = 4 Name = cyl1;box;cyl2, index = 5 Number of surface: nodes - 14210, elements - 28672 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.222901 Creating surface mesh ... Surface mesh seconds: 0.01594 Recovering boundaries... Boundary recovery seconds: 0.112199 Removing exterior tetrahedra ... Warning: The 3-th region point lies outside the convex hull. Spreading region attributes. Exterior tets removal seconds: 0.010649 Recovering Delaunayness... Delaunay recovery seconds: 0.152578 Refining mesh... Refinement seconds: 0.565914 Smoothing vertices... Mesh smoothing seconds: 0.857477 Improving mesh... Mesh improvement seconds: 0.032934 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.007917 Total running seconds: 1.97919 Statistics: Input points: 14210 Input facets: 28672 Input segments: 42880 Input holes: 0 Input regions: 3 Mesh points: 22401 Mesh tetrahedra: 122047 Mesh faces: 247637 Mesh faces on exterior boundary: 7086 Mesh faces on input facets: 28672 Mesh edges on input segments: 42880 Steiner points inside domain: 8191 Done meshing using TetGen! Writing vtk file .... Writing vtk general file .... Finished writing vtk file Writing exodus file .... Block: 'c_tet', blk_id 1, num_entries 27365 Block: 'b_tet', blk_id 2, num_entries 58342 Block: 'a_tet', blk_id 3, num_entries 36340 Sideset: 'box', set_id 1, num_entries 7086 Sideset: 'cyl1', set_id 2, num_entries 15896 Sideset: 'cyl2', set_id 3, num_entries 10762 Finished writing Exodus file real 0m7.007s user 0m4.205s sys 0m0.288s + status=0 + set +x ================================================= CAPS verification (using pyCAPS) case plato_aflr_tetgen_cyli_box_PyTest.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Did not run examples for: abaqus Nastran Mystran ================================================= All tests pass! ================================================= ================================================= ++ cd /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest ++ ./execute_PyTestRegression.sh STRUCTURE ================================================= Legacy Using python : /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/ESP/venv/bin/python ================================================= Running.... STRUCTURE PyTests ================================================= + rm -rf masstran_PyTest + echo 'masstran_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt masstran_PyTest.py test; + python -u masstran_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 1159 Number of elements = 798 Number of triangle elements = 0 Number of quadrilateral elements = 798 ---------------------------- Total number of nodes = 1159 Total number of elements = 798 No analysis directory provided - defaulting to altName 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 = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1159 Number of elements = 798 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 798 Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting results mass properties..... Area 3.428666259749 Mass 5383.006027806 Centroid [1.222256036872, 0.1634981473779, -4.647736192456e-11] CG [1.222256036872, 0.1634981473779, -4.647907951721e-11] Ixx 22133.97306031 Iyy 23448.30046704 Izz 1389.213122564 Ixy 164.2055275655 Ixz -7.485782319314e-06 Iyz 1.710545499156e-06 I [22133.97306031, 23448.30046704, 1389.213122564, 164.2055275655, -7.485782319314e-06, 1.710545499156e-06] II [[22133.97306031, -164.2055275655, 7.485782319314e-06], [-164.2055275655, 23448.30046704, -1.710545499156e-06], [7.485782319314e-06, -1.710545499156e-06, 1389.213122564]] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m5.139s user 0m6.715s sys 0m7.938s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf masstran_AGARD445_PyTest + echo 'masstran_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt masstran_AGARD445_PyTest.py test; + python -u masstran_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName 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 = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate Done getting FEA properties Updating mesh element types based on properties input Getting results mass properties..... Area 547.7004 Mass 0.01605224431138 Centroid [20.03586282449, 14.01686746988, 0.0] CG [20.03586282449, 14.01686746988, 0.0] Ixx 1.140246300554 Iyy 0.919317482675 Izz 2.059563783229 Ixy 0.7352134614013 Ixz 0.0 Iyz 0.0 I [1.140246300554, 0.919317482675, 2.059563783229, 0.7352134614013, 0.0, 0.0] II [[1.140246300554, -0.7352134614013, -0.0], [-0.7352134614013, 0.919317482675, -0.0], [-0.0, -0.0, 2.059563783229]] WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.472s user 0m0.533s sys 0m0.147s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case masstran_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf hsm_SingleLoadCase_PyTest + echo 'hsm_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt hsm_SingleLoadCase_PyTest.py test; + python -u hsm_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 81 Number of elements = 96 Elemental Tria3 = 0 Elemental Quad4 = 64 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 Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedPressure Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 32 ->HSMSOL Matrix Non-zero Entries = 5741 Converging HSM equation system ... iter dr dd dp rlx max 1 0.130E-01 0.165E+00 0.153E-04 1.000 ddy @ ( 0.25 0.06 0.00) 1* 0.260E-03 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 1* 0.240E-05 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.09 0.00) 2 0.379E-02 0.505E-01 0.750E-04 1.000 ddy @ ( 0.25 0.19 0.00) 2* 0.420E-04 0.000E+00 0.000E+00 1.000 drz @ ( 0.25 0.12 0.00) 3 0.168E-02 0.225E-01 0.208E-04 1.000 ddy @ ( 0.25 0.06 0.00) 4 0.325E-03 0.427E-02 0.250E-05 1.000 ddy @ ( 0.25 0.19 0.00) 5 0.794E-05 0.112E-03 0.170E-06 1.000 ddy @ ( 0.25 0.19 0.00) 6 0.387E-08 0.598E-07 0.197E-09 1.000 ddy @ ( 0.25 0.06 0.00) 7 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00) Converging n vectors ... it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 ) it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 ) Converging e1,e2 vectors ... it = 1 de = 0.691E-03 rlx = 1.000 ( 45 ) it = 2 de = 0.404E-04 rlx = 1.000 ( 9 ) it = 3 de = 0.142E-07 rlx = 1.000 ( 46 ) it = 4 de = 0.521E-11 rlx = 1.000 ( 62 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.685s user 0m0.802s sys 0m0.096s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf hsm_CantileverPlate_PyTest + echo 'hsm_CantileverPlate_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt hsm_CantileverPlate_PyTest.py test; + python -u hsm_CantileverPlate_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Creating HSM BEM Getting quads for BEM! Number of nodal coordinates = 40 Number of elements = 51 Elemental Tria3 = 0 Elemental Quad4 = 27 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 Getting FEA constraints....... Number of constraints - 1 Constraint name - edgeConstraint No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA loads....... Number of loads - 1 Load name - appliedLoad Done getting FEA loads Writing Nastran grid and connectivity file (in small field format) .... Finished writing Nastran grid file Max Adjacency set to = 9 MaxDim = 4, numBCEdge = 3, numBCNode = 4, numJoint = 0 NEED TO ADD MORE CODE TO hsm_setGlobalParameter NEED TO ADD MORE CODE TO hsm_setNodeBCParameter NumBCNode = 4 ->HSMSOL Matrix Non-zero Entries = 1313 Converging HSM equation system ... iter dr dd dp rlx max 1 0.314E+01 0.628E+01 0.000E+00 0.080 ddx @ ( 1.00 0.00 0.00) 1* 0.341E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.326E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 1* 0.438E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 2 0.274E+01 0.521E+01 0.106E-07 0.096 ddx @ ( 1.00 0.03 0.00) 2* 0.321E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 2* 0.373E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 2* 0.777E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3 0.202E+01 0.439E+01 0.928E-07 0.114 ddz @ ( 1.00 0.03 0.00) 3* 0.442E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.623E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 3* 0.163E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.07 0.00) 3* 0.167E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.03 0.00) 4 0.192E+01 0.476E+01 0.126E-07 0.105 ddz @ ( 1.00 0.03 0.00) 4* 0.335E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.332E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 4* 0.451E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 5 0.187E+01 0.394E+01 0.254E-07 0.127 ddz @ ( 1.00 0.07 0.00) 5* 0.353E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.379E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 5* 0.638E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6 0.156E+01 0.300E+01 0.112E-06 0.166 ddx @ ( 1.00 0.07 0.00) 6* 0.326E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 6* 0.575E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.193E-03 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 6* 0.272E-06 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7 0.103E+01 0.323E+01 0.345E-07 0.155 ddx @ ( 1.00 0.07 0.00) 7* 0.259E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.297E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 7* 0.435E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8 0.756E+00 0.259E+01 0.139E-07 0.193 ddx @ ( 1.00 0.03 0.00) 8* 0.295E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 8* 0.350E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 8* 0.587E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9 0.678E+00 0.179E+01 0.639E-07 0.279 ddx @ ( 0.89 0.00 0.00) 9* 0.330E-01 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 9* 0.457E-02 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.00 0.00) 9* 0.167E-03 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 9* 0.264E-06 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10 0.452E+00 0.171E+01 0.499E-07 0.292 ddz @ ( 1.00 0.10 0.00) 10* 0.166E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.239E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 10* 0.393E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) iter dr dd dp rlx max 11 0.257E+00 0.120E+01 0.614E-08 0.417 ddz @ ( 1.00 0.00 0.00) 11* 0.206E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.283E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 11* 0.488E-04 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12 0.131E+00 0.647E+00 0.288E-08 0.772 ddz @ ( 0.89 0.00 0.00) 12* 0.238E-01 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.357E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.10 0.00) 12* 0.849E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 13 0.393E-01 0.238E+00 0.325E-07 1.000 ddx @ ( 1.00 0.07 0.00) 13* 0.336E-02 0.000E+00 0.000E+00 1.000 drz @ ( 1.00 0.00 0.00) 13* 0.936E-04 0.000E+00 0.000E+00 1.000 drx @ ( 1.00 0.10 0.00) 14 0.475E-03 0.514E-02 0.635E-07 1.000 ddx @ ( 1.00 0.10 0.00) 15 0.893E-06 0.651E-06 0.135E-08 1.000 drx @ ( 1.00 0.00 0.00) 16 0.574E-10 0.216E-09 0.140E-11 1.000 ddx @ ( 0.44 0.00 0.00) 17 0.148E-15 0.575E-15 0.104E-14 1.000 dps @ ( 1.00 0.10 0.00) Converging n vectors ... it = 1 dn = 0.193E+01 rlx = 1.000 ( 9 ) it = 2 dn = 0.423E-15 rlx = 1.000 ( 31 ) Converging e1,e2 vectors ... it = 1 de = 0.285E+01 rlx = 0.351 ( 24 ) it = 2 de = 0.269E+01 rlx = 0.372 ( 14 ) it = 3 de = 0.202E+01 rlx = 0.494 ( 40 ) it = 4 de = 0.122E+01 rlx = 0.820 ( 40 ) it = 5 de = 0.378E+00 rlx = 1.000 ( 40 ) it = 6 de = 0.127E-01 rlx = 1.000 ( 14 ) it = 7 de = 0.524E-06 rlx = 1.000 ( 40 ) it = 8 de = 0.938E-16 rlx = 1.000 ( 22 ) Calculating strains, stress resultants ... Writing HSM solution to Tecplot File - HSMCantileverPlate.dat WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.716s user 0m0.606s sys 0m0.095s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case hsm_CantileverPlate_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Aeroelastic_PyTest + echo 'astros_Aeroelastic_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Aeroelastic_PyTest.py test; + python -u astros_Aeroelastic_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 = Rib_Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = Skin_Top, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Rib_Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 6 Name = Ribs, index = 1 Name = Skin, index = 2 Name = Spar1, index = 3 Name = Rib_Root, index = 4 Name = Spar2, index = 5 Name = Wing, index = 6 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 286 Number of elements = 386 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 92 Elemental Quad4 = 294 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 287 Combined Number of elements = 387 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 92 Combined Elemental Quad4 = 294 Getting vortex lattice surface data VLM surface name - Skin_Top Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 48 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 5 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Ribs No "material" specified for Property tuple Ribs, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, defaulting to an index of 1 Property name - Spar1 No "material" specified for Property tuple Spar1, defaulting to an index of 1 Property name - Spar2 No "material" specified for Property tuple Spar2, defaulting to an index of 1 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - ribSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Rib_Root No "groupName" specified for Connection tuple Rib_Root! Looking for automatic connections from the use of capsConnectLink for Rib_Root 30 automatic connections were made for capsConnect Rib_Root (node id 287) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim1 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing constraint cards--each subcase individually Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m10.043s user 0m13.578s sys 0m4.591s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Aeroelastic_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_AGARD445_PyTest + echo 'astros_AGARD445_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_AGARD445_PyTest.py test; + python -u astros_AGARD445_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 = constEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = yatesPlate, index = 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 36 Number of elements = 25 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 25 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Mahogany Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - yatesPlate 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 Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Running Astros...... Done running Astros! Getting results natural frequencies..... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 5.78 (Hz) Natural freq (Mode 2) = 30.66 (Hz) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.533s user 0m0.626s sys 0m0.166s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_AGARD445_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Composite_PyTest + echo 'astros_Composite_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Composite_PyTest.py test; + python -u astros_Composite_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = plate, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - plate Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plateTip, 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 15 Number of elements = 8 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 8 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" 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 - cantilever No "constraintType" specified for Constraint tuple cantilever, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.696s user 0m0.744s sys 0m0.170s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Composite_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_CompositeWingFreq_PyTest + echo 'astros_CompositeWingFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_CompositeWingFreq_PyTest.py test; + python -u astros_CompositeWingFreq_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt Mapping Csys attributes ................ Number of unique Csys attributes = 1 Name = wing, index = 1 Getting FEA coordinate systems....... Number of coordinate systems - 1 Coordinate system name - wing Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = root, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = wing, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = wing, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = wing, index = 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 Warning: No capsGroup/capsIgnore attribute found on edge 5 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 6 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 7 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 443 Number of elements = 845 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 845 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Aluminum No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic" Material name - Graphite_epoxy Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - wing Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - root No "constraintType" specified for Constraint tuple root, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Writing coordinate system cards Running Astros...... Done running Astros! Getting results for natural frequencies..... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 5.90553 (Hz) Natural freq (Mode 2) = 29.72860 (Hz) Natural freq (Mode 3) = 39.11840 (Hz) Natural freq (Mode 4) = 77.46400 (Hz) Natural freq (Mode 5) = 99.53050 (Hz) Natural freq (Mode 6) = 146.35200 (Hz) Natural freq (Mode 7) = 178.74700 (Hz) Natural freq (Mode 8) = 234.29900 (Hz) Natural freq (Mode 9) = 278.97300 (Hz) Natural freq (Mode 10) = 313.52300 (Hz) No variable name provided - all variables will be writen to file Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 Reading Astros OUT file - extracting Eigen-Vectors! Number of Eigen-Vectors = 10 Number of Grid Points = 443 for each Eigen-Vector Loading Eigen-Vector = 1 Loading Eigen-Vector = 2 Loading Eigen-Vector = 3 Loading Eigen-Vector = 4 Loading Eigen-Vector = 5 Loading Eigen-Vector = 6 Loading Eigen-Vector = 7 Loading Eigen-Vector = 8 Loading Eigen-Vector = 9 Loading Eigen-Vector = 10 WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.getAnalysisInfo' is deprecated. Please use 'Analysis.info'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsBound.writeTecplot' is deprecated. Please use 'vertexSet["name"].dataSet["variableName"].writeTecplot'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m44.823s user 0m37.096s sys 0m0.831s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_CompositeWingFreq_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Flutter_15degree + echo 'astros_Flutter_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Flutter_15degree.py test; + python -u astros_Flutter_15degree.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - Body Property name - Edge Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Flutter Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aero card Writing analysis cards Writing constraint cards--each subcase individually Writing material cards Writing property cards Writing unsteady aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.135s user 0m0.948s sys 0m0.329s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Flutter_15degree.py passed (as expected) ================================================= ================================================= + rm -rf astros_MultipleLoadCase_PyTest + echo 'astros_MultipleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_MultipleLoadCase_PyTest.py test; + python -u astros_MultipleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 16 Number of elements = 9 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 9 Aero_Reference value is NULL - No aero reference parameters set 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 - 5 Load name - load_0 Load name - load_1 Load name - load_2 Load name - load_3 Load name - load_4 Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 5 Analysis name - load_0 Analysis name - load_1 Analysis name - load_2 Analysis name - load_3 Analysis name - load_4 Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case load_0, assuming all constraints are applied!!!! Warning: No constraints specified for case load_1, assuming all constraints are applied!!!! Warning: No constraints specified for case load_2, assuming all constraints are applied!!!! Warning: No constraints specified for case load_3, assuming all constraints are applied!!!! Warning: No constraints specified for case load_4, assuming all constraints are applied!!!! Writing analysis cards Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load ADD cards Writing constraint cards--all constraints for each subcase Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.882s user 0m0.828s sys 0m0.180s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_MultipleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_PyTest + echo 'astros_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_PyTest.py test; + python -u astros_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 293 Number of elements = 217 Number of triangle elements = 0 Number of quadrilateral elements = 217 ---------------------------- Total number of nodes = 293 Total number of elements = 217 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 = Rib_Constraint, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = Ribs_and_Spars, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 293 Number of elements = 217 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 217 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 2 Material name - Madeupium Material name - Unobtainium No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - Ribs_and_Spars Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - ribConstraint No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Running Astros...... Done running Astros! Getting results for natural frequencies..... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 10 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Loading Eigen-Value = 3 Loading Eigen-Value = 4 Loading Eigen-Value = 5 Loading Eigen-Value = 6 Loading Eigen-Value = 7 Loading Eigen-Value = 8 Loading Eigen-Value = 9 Loading Eigen-Value = 10 Natural freq (Mode 1) = 0.02335 (Hz) Natural freq (Mode 2) = 0.02335 (Hz) Natural freq (Mode 3) = 0.11619 (Hz) Natural freq (Mode 4) = 0.11619 (Hz) Natural freq (Mode 5) = 0.14468 (Hz) Natural freq (Mode 6) = 0.14468 (Hz) Natural freq (Mode 7) = 0.23352 (Hz) Natural freq (Mode 8) = 0.23352 (Hz) Natural freq (Mode 9) = 0.30497 (Hz) Natural freq (Mode 10) = 0.30497 (Hz) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m16.258s user 0m14.640s sys 0m6.181s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_SingleLoadCase_PyTest + echo 'astros_SingleLoadCase_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_SingleLoadCase_PyTest.py test; + python -u astros_SingleLoadCase_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 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 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 12 Number of elements = 6 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 6 Aero_Reference value is NULL - No aero reference parameters set 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 Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Analysis tuple is NULL Getting FEA analyses....... Number of analyses - 1 Analysis name - Default Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.732s user 0m0.746s sys 0m0.177s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_SingleLoadCase_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBarFreq_PyTest + echo 'astros_ThreeBarFreq_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBarFreq_PyTest.py test; + python -u astros_ThreeBarFreq_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold 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 = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, defaulting to "ZeroDisplacement" Done getting FEA constraints Support tuple is NULL - No supports applied Connect tuple is NULL - Using defaults Load tuple is NULL - No loads applied Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - EigenAnalysis No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal" Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!! Writing analysis cards Writing constraint cards--all constraints for each subcase Writing material cards Writing property cards Running Astros...... Done running Astros! Getting results for natural frequencies..... Reading Astros OUT file - extracting Eigen-Values! Number of Eigen-Values = 2 Loading Eigen-Value = 1 Loading Eigen-Value = 2 Natural freq (Mode 1) = 86.13400 (Hz) Natural freq (Mode 2) = 168.53300 (Hz) WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.748s user 0m0.809s sys 0m0.177s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBarFreq_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBarLinkDesign_PyTest + echo 'astros_ThreeBarLinkDesign_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBarLinkDesign_PyTest.py test; + python -u astros_ThreeBarLinkDesign_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold 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 = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, 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 - appliedForce Done getting FEA loads Getting FEA design variables....... Number of design variables - 3 Design_Variable name - Bar1A Design_Variable name - Bar2A Design_Variable name - Bar3A Design_Variable_Relation name - Bar1A Design_Variable_Relation name - Bar2A Design_Variable_Relation name - Bar3A Number of design variable relations - 3 Done getting FEA design variables Getting FEA design constraints....... Number of design constraints - 3 Design_Constraint name - stress1 Design_Constraint name - stress2 Design_Constraint name - stress3 Done getting FEA design constraints 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 Mass_Increment tuple is NULL - No mass increments applied Design_Response tuple is NULL - No design responses applied Design_Equation_Response tuple is NULL - No design equation responses applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Nastran grid and connectivity file (in large field format) .... Finished writing Nastran grid file Writing subElement types (if any) - appending mesh file Writing mass increment set Writing Nastran instruction file.... Writing mass increment cards Writing analysis cards, 0 Writing load ADD cards Writing constraint ADD cards Writing design constraint ADD cards Writing load cards Writing constraint cards Writing material cards Writing property cards Writing design variable cards Writing design variable relation cards Writing design constraints and responses cards Done writing aeroelastic cards Done writing files Running Astros...... Done running Astros! Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py", line 212, in <module> nastranAIM.postAnalysis() File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis self._analysisObj.postAnalysis() File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed return func(*args, **kwargs) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 2914, in postAnalysis if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs)) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus raise CAPSError(status, msg=msg, errors=errors) pyCAPS.caps.CAPSError: CAPS_IOERR: ================================================================================ nastranAIM.c:3037 in aimPostAnalysis(): Error: Unable to open file: threebar_nastran_Test.f06 ================================================================================ WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! real 0m0.621s user 0m0.581s sys 0m0.212s + status=1 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBarLinkDesign_PyTest.py failed (as NOT expected) ================================================= ================================================= + rm -rf astros_ThreeBarMultiLoad_PyTest + echo 'astros_ThreeBarMultiLoad_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBarMultiLoad_PyTest.py test; + python -u astros_ThreeBarMultiLoad_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold 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 = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 2 Constraint name - conOne No "constraintType" specified for Constraint tuple conOne, defaulting to "ZeroDisplacement" Constraint name - conTwo No "constraintType" specified for Constraint tuple conTwo, 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 - 2 Load name - loadOne Load name - loadTwo Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 2 Analysis name - analysisOne Analysis name - analysisTwo Done getting FEA analyses Writing Astros grid and connectivity file (in large field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.745s user 0m0.793s sys 0m0.201s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBarMultiLoad_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_ThreeBar_PyTest + echo 'astros_ThreeBar_PyTest.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_ThreeBar_PyTest.py test; + python -u astros_ThreeBar_PyTest.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt WARNING:: WireBody is non-manifold 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 = boundary, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = force, 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 capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = bar1, index = 1 Name = bar2, index = 2 Name = bar3, index = 3 capsIgnore attribute found for edge - 3!! capsIgnore attribute found. Removing unneeded nodes and elements from mesh! Removing unused nodes... Removed 0 (out of 4) unused nodes! Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4 Number of elements = 3 Elemental Nodes = 0 Elemental Rods = 3 Elemental Tria3 = 0 Elemental Quad4 = 0 Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - Madeupium Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - bar1 Property name - bar2 Property name - bar3 Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - BoundaryCondition No "constraintType" specified for Constraint tuple BoundaryCondition, 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 - appliedForce Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - SingleLoadCase Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing Astros instruction file.... Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing material cards Writing property cards Running Astros...... Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m0.704s user 0m0.743s sys 0m0.195s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_ThreeBar_PyTest.py passed (as expected) ================================================= ================================================= + rm -rf astros_Trim_15degree + echo 'astros_Trim_15degree.py test;' + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt astros_Trim_15degree.py test; + python -u astros_Trim_15degree.py -verbosity=0 -workDir=runDirectory + tee -a /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/STRUCTURE/DARWIN_ARM64/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt 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 = Root_Point, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = Root_Point, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 1 Name = WingSurface, index = 1 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 1 Name = Root, index = 1 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping capsReference attributes ................ Number of unique capsReference attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 4 Name = Edge, index = 1 Name = Body, index = 2 Name = Root, index = 3 Name = Wing, index = 4 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 96 Number of elements = 77 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 77 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Combining multiple FEA meshes! Combined Number of nodal coordinates = 97 Combined Number of elements = 78 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 77 Getting vortex lattice surface data VLM surface name - WingSurface Done getting vortex lattice surface data Getting FEA vortex lattice mesh Surface 1: Number of points found for aero-spline = 96 (Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces ! Aero_Reference value is NULL - No aero reference parameters set Getting FEA materials....... Number of materials - 1 Material name - aluminum No "materialType" specified for Material tuple aluminum, defaulting to "Isotropic" Done getting FEA materials Getting FEA properties....... Number of properties - 3 Property name - Body Property name - Edge Property name - Root Done getting FEA properties Updating mesh element types based on properties input Getting FEA constraints....... Number of constraints - 1 Constraint name - PointConstraint No "constraintType" specified for Constraint tuple PointConstraint, defaulting to "ZeroDisplacement" Done getting FEA constraints Getting FEA supports....... Number of supports - 1 Support name - PointSupport Done getting FEA supports Getting FEA connections....... Number of connection tuples - 1 Connection name - Root No "groupName" specified for Connection tuple Root! Looking for automatic connections from the use of capsConnectLink for Root 8 automatic connections were made for capsConnect Root (node id 97) Done getting FEA connections Getting FEA loads....... Number of loads - 2 Load name - GravityLoad No "groupName" specified for Load tuple GravityLoad, going to use load name Load name - PointLoad Done getting FEA loads Optimization Control tuple is NULL - Default optimization control is used Getting FEA optimization control....... Done getting FEA Optimization Control Design_Variable tuple is NULL - No design variables applied Design_Constraint tuple is NULL - No design constraints applied Getting FEA analyses....... Number of analyses - 1 Analysis name - Trim Done getting FEA analyses Writing Astros grid and connectivity file (in free field format) .... Finished writing Astros grid file Writing subElement types (if any) - appending mesh file Writing connection cards - appending mesh file Writing Astros instruction file.... Writing aeros card Writing analysis cards Writing load ADD cards Writing constraint cards--each subcase individually Writing load cards Writing support cards Writing material cards Writing property cards Writing aeroelastic cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG Done running Astros! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'! real 0m1.128s user 0m0.986s sys 0m0.279s + status=0 + set +x ================================================= Legacy CAPS verification (using pyCAPS) case astros_Trim_15degree.py passed (as expected) ================================================= ************************************************* ************************************************* ================================================= Legacy Did not run examples for: Nastran Mystran ================================================= ================================================= Legacy Summary of examples NOT finished as expected astros_ThreeBarLinkDesign_PyTest.py See pyCAPSlog.txt for more details. ================================================= ================================================= ================================================= Build step 'Conditional step (single)' marked build as failure [GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is '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