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Skipping 1,581 KB.. Full LogDGEOM : Nodes,Faces,BEdges= 1523 3038 476 OVERALL : CPU Time = 0.079 seconds Body 1 (of 2) Number of nodes = 304 Number of elements = 604 Number of triangle elements = 604 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1523 Total number of elements = 3038 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 3 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 EGADS : 2 1 3 -2 -3 EGADS : 3 2 EGADS : 4 4 5 -6 -7 EGADS : 5 -8 11 10 -9 EGADS : 6 12 8 -13 -4 EGADS : 7 -14 6 15 -10 EGADS : 8 7 14 -11 -12 EGADS : 9 -5 13 9 -15 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 EGADS : 2 Yes 1 3 -2 -3 EGADS : 3 Yes 2 EGADS : 4 Yes 4 5 -6 -7 EGADS : 5 Yes -8 11 10 -9 EGADS : 6 Yes 12 8 -13 -4 EGADS : 7 Yes -14 6 15 -10 EGADS : 8 Yes 7 14 -11 -12 EGADS : 9 Yes -5 13 9 -15 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 1 1 1 1 2 EGADS : 2 0 Yes 2 2 1 2 3 EGADS : 3 0 Yes 1 2 1 2 2 EGADS : 4 1 Yes 4 3 NA 4 6 EGADS : 5 1 Yes 3 5 NA 4 9 EGADS : 6 1 Yes 6 5 NA 4 7 EGADS : 7 1 Yes 4 6 NA 4 8 EGADS : 8 1 Yes 8 7 NA 5 6 EGADS : 9 1 Yes 7 9 NA 5 9 EGADS : 10 1 Yes 10 9 NA 5 7 EGADS : 11 1 Yes 8 10 NA 5 8 EGADS : 12 1 Yes 4 8 NA 6 8 EGADS : 13 1 Yes 3 7 NA 6 9 EGADS : 14 1 Yes 6 10 NA 7 8 EGADS : 15 1 Yes 5 9 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 2 0 0.5 EGADS : 2 Yes 3 0 0.5 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 100 167 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 105 177 0 AFLR4 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1737 3466 512 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1737 3466 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 391 698 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1738 3468 512 OVERALL : CPU Time = 0.087 seconds Body 1 (of 2) Number of nodes = 519 Number of elements = 1034 Number of triangle elements = 1034 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1738 Total number of elements = 3468 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 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 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 3 8 -11 EGADS : 5 Yes 4 10 -12 -5 EGADS : 6 Yes -6 12 11 -9 EGADS : 7 Yes -13 14 15 -16 EGADS : 8 Yes -17 18 13 -19 EGADS : 9 Yes 20 22 -21 -14 EGADS : 10 Yes -15 23 17 -24 EGADS : 11 Yes 16 24 19 EGADS : 12 Yes 25 26 -20 -18 EGADS : 13 Yes 21 27 -25 -23 EGADS : 14 Yes -22 -26 -27 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 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.60986 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 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 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD 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 : 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= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 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= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17058 33386 0 AFLR4 : Nodes, Trias,Quads= 7507 14284 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 17154 33578 0 AFLR4 : Nodes, Trias,Quads= 7368 14006 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14987 29245 0 AFLR4 : Nodes, Trias,Quads= 6879 13029 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 330 546 0 AFLR4 : Nodes, Trias,Quads= 322 530 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14793 28857 0 AFLR4 : Nodes, Trias,Quads= 6844 12959 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 328 542 0 AFLR4 : Nodes, Trias,Quads= 324 534 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 28462 56916 3616 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 28462 56916 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= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 15590 30449 0 AFLR4 : Nodes, Trias,Quads= 9447 18163 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15870 31009 0 AFLR4 : Nodes, Trias,Quads= 9439 18147 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14689 28649 0 AFLR4 : Nodes, Trias,Quads= 9247 17765 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 346 577 0 AFLR4 : Nodes, Trias,Quads= 359 603 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14582 28435 0 AFLR4 : Nodes, Trias,Quads= 9309 17889 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 348 581 0 AFLR4 : Nodes, Trias,Quads= 361 607 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 37391 74774 3650 OVERALL : CPU Time = 2.660 seconds Body 1 (of 1) Number of nodes = 37391 Number of elements = 74774 Number of triangle elements = 74774 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 37391 Total number of elements = 74774 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 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 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes 1 2 -3 -4 EGADS : 2 Yes 5 6 -7 -1 EGADS : 3 Yes -2 7 9 -8 EGADS : 4 Yes -10 3 8 -11 EGADS : 5 Yes 4 10 -12 -5 EGADS : 6 Yes -6 12 11 -9 EGADS : 7 Yes -13 14 15 -16 EGADS : 8 Yes -17 18 13 -19 EGADS : 9 Yes 20 22 -21 -14 EGADS : 10 Yes -15 23 17 -24 EGADS : 11 Yes 16 24 19 EGADS : 12 Yes 25 26 -20 -18 EGADS : 13 Yes 21 27 -25 -23 EGADS : 14 Yes -22 -26 -27 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 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 15.2197 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 AFLR4 : Global Scale Factor = 2 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 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD 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 : 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= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 37 52 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6308 12196 0 AFLR4 : Nodes, Trias,Quads= 3150 5880 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6486 12552 0 AFLR4 : Nodes, Trias,Quads= 3253 6086 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5848 11277 0 AFLR4 : Nodes, Trias,Quads= 3043 5667 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 250 400 0 AFLR4 : Nodes, Trias,Quads= 245 390 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5864 11309 0 AFLR4 : Nodes, Trias,Quads= 3002 5585 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 249 398 0 AFLR4 : Nodes, Trias,Quads= 244 388 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 12267 24526 2204 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 12267 24526 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 41 60 0 AFLR4 : Nodes, Trias,Quads= 36 50 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6119 11815 0 AFLR4 : Nodes, Trias,Quads= 4216 8009 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 226 328 0 AFLR4 : Nodes, Trias,Quads= 122 120 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6177 11933 0 AFLR4 : Nodes, Trias,Quads= 4307 8193 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5886 11351 0 AFLR4 : Nodes, Trias,Quads= 4129 7837 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 250 401 0 AFLR4 : Nodes, Trias,Quads= 252 405 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 225 326 0 AFLR4 : Nodes, Trias,Quads= 122 120 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5948 11476 0 AFLR4 : Nodes, Trias,Quads= 4168 7916 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 246 394 0 AFLR4 : Nodes, Trias,Quads= 244 390 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 16649 33290 2234 OVERALL : CPU Time = 2.079 seconds Body 1 (of 1) Number of nodes = 16649 Number of elements = 33290 Number of triangle elements = 33290 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 16649 Total number of elements = 33290 . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 2 Faces EGADS : Body 0 has 6 Edges EGADS : Body 0 has 2 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 0 0 1 0 1 1 EGADS : 3 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 4 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 5 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 6 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 7 Yes 1 0 1 NA NA 3 4 5 6 EGADS : 8 Yes 1 0 1 NA NA 3 4 5 6 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 -2 3 4 EGADS : 2 -5 -4 6 2 EGADS : 3 7 8 -9 -10 EGADS : 4 -11 14 13 -12 EGADS : 5 15 11 -16 -7 EGADS : 6 -17 9 18 -13 EGADS : 7 10 17 -14 -15 EGADS : 8 -8 16 12 -18 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 -2 3 4 EGADS : 2 Yes -5 -4 6 2 EGADS : 3 Yes 7 8 -9 -10 EGADS : 4 Yes -11 14 13 -12 EGADS : 5 Yes 15 11 -16 -7 EGADS : 6 Yes -17 9 18 -13 EGADS : 7 Yes 10 17 -14 -15 EGADS : 8 Yes -8 16 12 -18 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 DEGEN 1 1 - 1 EGADS : 2 0 Yes 2 1 1 1 2 EGADS : 3 0 DEGEN 2 2 - 1 EGADS : 4 0 Yes 2 1 1 1 2 EGADS : 5 0 DEGEN 1 1 - 2 EGADS : 6 0 DEGEN 2 2 - 2 EGADS : 7 1 Yes 4 3 NA 3 5 EGADS : 8 1 Yes 3 5 NA 3 8 EGADS : 9 1 Yes 6 5 NA 3 6 EGADS : 10 1 Yes 4 6 NA 3 7 EGADS : 11 1 Yes 8 7 NA 4 5 EGADS : 12 1 Yes 7 9 NA 4 8 EGADS : 13 1 Yes 10 9 NA 4 6 EGADS : 14 1 Yes 8 10 NA 4 7 EGADS : 15 1 Yes 4 8 NA 5 7 EGADS : 16 1 Yes 3 7 NA 5 8 EGADS : 17 1 Yes 6 10 NA 6 7 EGADS : 18 1 Yes 5 9 NA 6 8 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 8.5 0 0.5 EGADS : 2 Yes 8.5 0 0 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 202 370 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 201 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1590 3172 432 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1590 3172 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 203 374 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 200 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1592 3176 428 OVERALL : CPU Time = 0.082 seconds Body 1 (of 2) Number of nodes = 373 Number of elements = 742 Number of triangle elements = 742 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1592 Total number of elements = 3176 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 1 Faces EGADS : Body 0 has 2 Edges EGADS : Body 0 has 1 Loops EGADS : Body 0 has 1 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 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 EGADS : 2 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 3 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 4 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 5 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 6 Yes 1 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 1 0 1 NA NA 2 3 4 5 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 1 -2 EGADS : 2 3 4 -5 -6 EGADS : 3 -7 10 9 -8 EGADS : 4 11 7 -12 -3 EGADS : 5 -13 5 14 -9 EGADS : 6 6 13 -10 -11 EGADS : 7 -4 12 8 -14 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 : Loop Edges Information EGADS : Loop Active Edges EGADS : 1 Yes -1 2 1 -2 EGADS : 2 Yes 3 4 -5 -6 EGADS : 3 Yes -7 10 9 -8 EGADS : 4 Yes 11 7 -12 -3 EGADS : 5 Yes -13 5 14 -9 EGADS : 6 Yes 6 13 -10 -11 EGADS : 7 Yes -4 12 8 -14 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 1 1 1 1 1 EGADS : 2 0 Yes 1 1 1 1 1 EGADS : 3 1 Yes 3 2 NA 2 4 EGADS : 4 1 Yes 2 4 NA 2 7 EGADS : 5 1 Yes 5 4 NA 2 5 EGADS : 6 1 Yes 3 5 NA 2 6 EGADS : 7 1 Yes 7 6 NA 3 4 EGADS : 8 1 Yes 6 8 NA 3 7 EGADS : 9 1 Yes 9 8 NA 3 5 EGADS : 10 1 Yes 7 9 NA 3 6 EGADS : 11 1 Yes 3 7 NA 4 6 EGADS : 12 1 Yes 2 6 NA 4 7 EGADS : 13 1 Yes 5 9 NA 5 6 EGADS : 14 1 Yes 4 8 NA 5 7 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 7.25 0 0 EGADS : 2 Yes 0 0 2 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 0 2 2 EGADS : 5 Yes 0 2 0 EGADS : 6 Yes 14 0 2 EGADS : 7 Yes 14 0 0 EGADS : 8 Yes 14 2 2 EGADS : 9 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.5 AFLR4 : Min Ref Bounding Box Length = 0.5 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 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 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD 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 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 919 1710 0 AFLR4 : Nodes, Trias,Quads= 675 1222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1830 3656 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1830 3656 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 930 1730 0 AFLR4 : Nodes, Trias,Quads= 728 1326 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1882 3760 496 OVERALL : CPU Time = 0.187 seconds Body 1 (of 2) Number of nodes = 663 Number of elements = 1326 Number of triangle elements = 1326 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1882 Total number of elements = 3760 .No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 46 Number of elements = 44 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 44 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 = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Rib_Root, index = 1 Name = Skin, index = 2 Name = Wing, index = 3 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 1 Number of elements = 1 Elemental Nodes = 1 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 0 Setting FEA Data Mesh for body = 1 Number of nodal coordinates = 46 Number of elements = 44 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 44 Combining multiple FEA meshes! Combined Number of nodal coordinates = 47 Combined Number of elements = 45 Combined Elemental Nodes = 1 Combined Elemental Rods = 0 Combined Elemental Tria3 = 0 Combined Elemental Quad4 = 44 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 = 3 Surface 2: Number of points found for aero-spline = 6 (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 - 2 Property name - Rib_Root No "material" specified for Property tuple Rib_Root, defaulting to an index of 1 Property name - Skin No "material" specified for Property tuple Skin, 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 8 automatic connections were made for capsConnect Rib_Root (node id 1) 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_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! .No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = plate, index = 1 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping 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 = 25 Number of elements = 16 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 16 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 .... 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 IEEE_DENORMAL Done running Astros! 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 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 cards Writing material cards Writing property cards Running Astros...... Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL Done running Astros! 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 IEEE_DENORMAL Done running Astros! .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp Writing mass properties file: caps.mass Parsing MassProp . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_1 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... Running avl...... Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_2 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - VTail1 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - VTail2 No "groupName" variable provided or no matches found, going to use tuple name VLM surface name - Wing Done getting vortex lattice surface data Writing surface - VTail1 (ID = 0) Section 1 of 2 (ID = 1) Section 2 of 2 (ID = 0) Writing surface - VTail2 (ID = 1) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Writing surface - Wing (ID = 2) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Running avl...... . Analysis object with the name, avlAIM, has already been initilized An altName of avlAIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 5 Name = Wing, index = 1 Name = hTail, index = 2 Name = vTail, index = 3 Name = VTail1, index = 4 Name = VTail2, index = 5 Getting vortex lattice surface data VLM surface name - Wing VLM surface name - hTail VLM surface name - vTail No "groupName" variable provided or no matches found, going to use tuple name Done getting vortex lattice surface data Writing surface - Wing (ID = 0) Section 1 of 4 (ID = 3) Section 2 of 4 (ID = 2) Section 3 of 4 (ID = 1) Section 4 of 4 (ID = 0) Writing surface - hTail (ID = 1) Section 1 of 3 (ID = 2) Section 2 of 3 (ID = 1) Section 3 of 3 (ID = 0) Writing surface - vTail (ID = 2) Section 1 of 2 (ID = 0) Section 2 of 2 (ID = 1) Running avl...... .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 9610 Number of elements = 19216 Number of triangle elements = 19216 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6142 Number of elements = 12280 Number of triangle elements = 12280 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 105 Number of elements = 206 Number of triangle elements = 206 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15857 Total number of elements = 31702 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9605 Number of elements = 19202 Number of triangle elements = 19202 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9605 Total number of elements = 19202 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62031) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 8) Getting surface mesh for body 2 (of 8) Getting surface mesh for body 3 (of 8) Getting surface mesh for body 4 (of 8) Getting surface mesh for body 5 (of 8) Getting surface mesh for body 6 (of 8) 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 70000A0CE000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 70000A0CE000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 7 (of 8) Getting surface mesh for body 8 (of 8) Body 1 (of 8) Number of nodes = 1538 Number of elements = 3072 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 8) Number of nodes = 901 Number of elements = 1798 Number of triangle elements = 1798 Number of quadrilateral elements = 0 Body 3 (of 8) Number of nodes = 1334 Number of elements = 2664 Number of triangle elements = 2664 Number of quadrilateral elements = 0 Body 4 (of 8) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 8) Number of nodes = 824 Number of elements = 1644 Number of triangle elements = 1644 Number of quadrilateral elements = 0 Body 6 (of 8) Number of nodes = 1958 Number of elements = 3916 Number of triangle elements = 3916 Number of quadrilateral elements = 0 Body 7 (of 8) Number of nodes = 942 Number of elements = 1880 Number of triangle elements = 1880 Number of quadrilateral elements = 0 Body 8 (of 8) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 83275 Total number of elements = 166526 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_1 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1538 Number of elements = 3072 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75268 Total number of elements = 150528 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_2 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = boxhole, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) 70000A0CE000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 70000A0CE000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1958 Number of elements = 3916 Number of triangle elements = 3916 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75688 Total number of elements = 151372 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 942 Number of elements = 1880 Number of triangle elements = 1880 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74672 Total number of elements = 149336 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cone, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1334 Number of elements = 2664 Number of triangle elements = 2664 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75064 Total number of elements = 150120 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 901 Number of elements = 1798 Number of triangle elements = 1798 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74631 Total number of elements = 149254 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 9605 Number of elements = 19202 Number of triangle elements = 19202 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9605 Total number of elements = 19202 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 1) Body 1 (of 1) Number of nodes = 7161 Number of elements = 14314 Number of triangle elements = 14314 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7161 Total number of elements = 14314 . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 824 Number of elements = 1644 Number of triangle elements = 1644 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74554 Total number of elements = 149100 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_7 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 2048 Number of elements = 4096 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75778 Total number of elements = 151552 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7819 Number of elements = 15634 Number of triangle elements = 15634 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 516 Number of elements = 1028 Number of triangle elements = 1028 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14224 Total number of elements = 28436 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14224, elements - 28436 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.33656 Creating surface mesh ... Surface mesh seconds: 0.073706 Recovering boundaries... Boundary recovery seconds: 0.177052 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.086076 Recovering Delaunayness... Delaunay recovery seconds: 0.092515 Refining mesh... 18960 insertions, added 14017 points, 701008 tetrahedra in queue. 6313 insertions, added 2494 points, 554976 tetrahedra in queue. 8415 insertions, added 1753 points, 70 tetrahedra in queue. Refinement seconds: 4.69189 Smoothing vertices... Mesh smoothing seconds: 4.59181 Improving mesh... Mesh improvement seconds: 0.196674 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.02745 Total running seconds: 10.2749 Statistics: Input points: 14224 Input facets: 28436 Input segments: 42654 Input holes: 2 Input regions: 0 Mesh points: 33058 Mesh tetrahedra: 159464 Mesh faces: 333146 Mesh faces on exterior boundary: 28436 Mesh faces on input facets: 28436 Mesh edges on input segments: 42654 Steiner points inside domain: 18834 Done meshing using TetGen! Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_1 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_2 will be used! Getting CFD boundary conditions Boundary condition name - Wing1 Warning: No boundary condition specified for capsGroup Wing2! Warning: No boundary condition specified for capsGroup Farfield! Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml ..... Error: Python error occurred while writing namelist file Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream self._update_tokens() File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 797, in _update_tokens next_token = next(self.tokens) ^^^^^^^^^^^^^^^^^ StopIteration During handling of the above exception, another exception occurred: Traceback (most recent call last): File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read return parser.read(nml_path) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 281, in read return self._readstream(nml_file, nml_patch) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 380, in _readstream raise ValueError( ValueError: End-of-file before end of namelist group: '&badNamelist' . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_3 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found! Creating namelist Done writing nml file with Python Info: No recognized data transfer names found. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml ..... Appending namelist Done writing nml file with Python Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_4 will be used! Getting CFD boundary conditions Boundary condition name - Wing1 . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_5 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_6 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Python library was linked, but will not be used! Writing MAPBC file .... Finished writing MAPBC file Warning: The fun3d.nml file will be overwritten! Writing fun3d.nml Info: No recognized data transfer names found. . Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_7 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Getting CFD design variables....... Number of design variables - 1 Design Variable name - Alpha Done getting CFD design variables Getting CFD functional....... Number of design variables - 1 Objective name - LoD Done getting CFD functional Python library was linked, but will not be used! Creating FUN3D directory tree Writing rubber.data Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Reading rubber.data .Closing fun3d!!!! 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 = 0 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 = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .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 = 0 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 = box1, index = 1 Face 3 TFI quading disabled with attribute .qParams Face 6 TFI quading disabled with attribute .qParams Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4009 Number of elements = 6570 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5126 Elemental Quad4 = 1444 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .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 = 0 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 = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input .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 = 0 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 = box1, 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 = 400 Number of elements = 361 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 361 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7819 Number of elements = 15634 Number of triangle elements = 15634 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5889 Number of elements = 11774 Number of triangle elements = 11774 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 516 Number of elements = 1028 Number of triangle elements = 1028 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14224 Total number of elements = 28436 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Number of surface: nodes - 14224, elements - 28436 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.337106 Creating surface mesh ... Surface mesh seconds: 0.06599 Recovering boundaries... Boundary recovery seconds: 0.176765 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.082471 Recovering Delaunayness... Delaunay recovery seconds: 0.096548 Refining mesh... 18960 insertions, added 14017 points, 701008 tetrahedra in queue. 6313 insertions, added 2494 points, 554976 tetrahedra in queue. 8415 insertions, added 1753 points, 70 tetrahedra in queue. Refinement seconds: 4.6987 Smoothing vertices... Mesh smoothing seconds: 4.47221 Improving mesh... Mesh improvement seconds: 0.211451 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.030729 Total running seconds: 10.1731 Statistics: Input points: 14224 Input facets: 28436 Input segments: 42654 Input holes: 2 Input regions: 0 Mesh points: 33058 Mesh tetrahedra: 159464 Mesh faces: 333146 Mesh faces on exterior boundary: 28436 Mesh faces on input facets: 28436 Mesh edges on input segments: 42654 Steiner points inside domain: 18834 Done meshing using TetGen! Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_1 will be used! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Wing1 . Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_2 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.1)" . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... Running xFoil...... . ---------------------------------------------------------------------- Ran 67 tests in 207.233s OK (skipped=10) WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'! WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! Legacy AIM unit testing done! (cd test; ./runUnitTest.sh) EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close! aimTransferUtil Tests passed! real 0m1.470s user 0m1.142s sys 0m0.094s ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7! Returning a 'NaN' string. Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7! Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00 Returning a 'NaN' string. Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00 Returning a 'NaN' string. Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6 Returning a 'NaN' string. Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6 Returning a 'NaN' string. Error in convert_integerToString: fieldWidth > 15 not verified Returning a 'NaN' string. Error in convert_integerToString: fieldWidth <= 0 Returning a 'NaN' string. Error in convert_integerToString: fieldWidth <= 0 Returning a 'NaN' string. miscUtils Tests passed! real 0m1.278s user 0m1.061s sys 0m0.088s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest vlmUtils Tests passed! real 0m1.274s user 0m1.061s sys 0m0.083s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest passed (as expected) ============================================= + rm -rf aimTest + expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm Root Path = /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch testingAIM/aimInitialize instance = -1 unitSys = (null)! caps_queryAnalysis = 0 4 3 1 testingAIM/aimInputs instance = -1 index = 1! in 1: testingAIMin 0 testingAIM/aimInputs instance = -1 index = 2! in 2: table 0 testingAIM/aimInputs instance = -1 index = 3! in 3: tessIn 0 testingAIM/aimInputs instance = -1 index = 4! in 4: meshFile 0 testingAIM/aimOutputs instance = -1 index = 1! out 1: testingAIMout 0 testingAIM/aimOutputs instance = -1 index = 2! out 2: tessOut 0 testingAIM/aimOutputs instance = -1 index = 3! out 3: meshFile 0 testingAIM/aimInitialize instance = 0 unitSys = m! testingAIM/aimInputs instance = 0 index = 1! testingAIM/aimInputs instance = 0 index = 2! testingAIM/aimInputs instance = 0 index = 3! testingAIM/aimInputs instance = 0 index = 4! testingAIM/aimOutputs instance = 0 index = 1! testingAIM/aimOutputs instance = 0 index = 2! testingAIM/aimOutputs instance = 0 index = 3! testingAIM/aimBackdoor instance = 0: Input String! Backdoor return string = aimBackdoor Output testingAIM/aimInitialize instance = 1 unitSys = (null)! testingAIM/aimInputs instance = 1 index = 1! testingAIM/aimInputs instance = 1 index = 2! testingAIM/aimInputs instance = 1 index = 3! testingAIM/aimInputs instance = 1 index = 4! testingAIM/aimOutputs instance = 1 index = 1! testingAIM/aimOutputs instance = 1 index = 2! testingAIM/aimOutputs instance = 1 index = 3! Intent = child APath = /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch/testingAIM1 UnitSys = (null) Exec = 1 Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0) Dirty = 3 Problem: # Dirty Analyses = 2! Bound: # Dirty Analyses = 2! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 1! testingAIM/aimUpdateState instance = 0! tess is NULL! testingAIM/aimPreAnalysis instance = 0! testingAIM/aimPreAnalysis aim_getBounds = 0 Analysis in Bound = Interface aim_newGeometry = 0! getDiscr = 0 getDataSet = 0, rank = 1, method = 0 0 scalars! meshRef = NULL testingAIM/aimExecute instance = 0! testingAIM/aimPostAnalysis instance = 0 restart = 0! testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter After Execute on Parent Problem: # Dirty Analyses = 1! Bound: # Dirty Analyses = 1! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 0! testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0! tessPtr = 0 testingAIM/aimUpdateState instance = 1! tess is NULL! testingAIM/aimDiscr: tname = Interface, instance = 1! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 3 matches Interface! testingAIM/aimDiscr: ntris = 1962! testingAIM/aimDiscr: npts = 1040! testingAIM/aimDiscr: tname = Interface, instance = 0! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 6 matches Interface! testingAIM/aimDiscr: ntris = 790! testingAIM/aimDiscr: npts = 442! testingAIM/aimTransfer name = scalar instance = 0 npts = 442/1! CAPS Info: Bound 'Interface' Normalized Integrated 'scalar' Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 3.844036e-11 testingAIM/aimPreAnalysis instance = 1! testingAIM/aimPreAnalysis aim_getBounds = 0 Analysis in Bound = Interface aim_newGeometry = 0! getDiscr = 0 getDataSet = -303, rank = 0, method = 0 vectors not setup yet! testingAIM/aimExecute instance = 1! testingAIM/aimPostAnalysis instance = 1 restart = 0! Dirty = 0 Problem: # Dirty Analyses = 0! Bound: # Dirty Analyses = 0! Analys0: # Dirty Analyses = 0! Analys1: # Dirty Analyses = 0! Body 1 has length units = cm Body 2 has length units = cm aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds ParamName has type VALUE, subtype PARAMETER with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 2 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 2 value = 0.000000 (null) Param has type VALUE, subtype PARAMETER with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 3 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 3 value = 99 (null) num has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 6 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 6 value = 8.000000 (null) x has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null) ymin has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null) zmin has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null) zmax has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null) unused has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 7 hist: (null) -> Initial Phase aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 1 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 16 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 16 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 value (1x3) = 1: Entry1 -> Value1 2: Entry2 -> Value2 3: Entry3 -> Value3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 8 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 9 testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0! aim_getDiscr 0 on Interface = 0 aim_getDataSet 0 on Interface = -329 value = 12.340000 cm lazy: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 10 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 12 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 12 value (1x3) = 1: Entry1 -> newValue1 2: Entry2 -> newValue2 3: Entry3 -> newValue3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 18 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 13 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 10 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 10 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 11 testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0! aim_getDiscr 1 on Interface = 0 aim_getDataSet 1 on Interface = -329 value = 12.340000 cm lazy: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 600001acc8c0 value = 600001acc8c0 ego lazy: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 14 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:51 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 1040 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 1040 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 26 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 15 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:19:12 26 1040 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 442 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 23 442 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 25 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Child Execute aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:52 25 442 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 hist: (null) -> Starting aimTest macys.mit.edu:66832 jenkins 2024/05/15 23:18:48 0 testingAIM/aimTransfer name = vector instance = 0 npts = 442/3! 442 points, rank=3, units=(null) 1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 8: 14.400000 14.400000 14.400000 14.400000 14.400000 14.381076 14.400000 15: 14.400000 14.385654 14.400000 14.386399 14.400000 14.400000 14.400000 22: 14.400000 14.400000 14.400000 14.383470 14.400000 14.400000 14.400000 29: 14.400000 14.390663 14.400000 14.400000 14.400000 14.400000 14.400000 36: 14.400000 14.400000 14.390526 14.400000 14.400000 14.400000 14.400000 43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 57: 14.400000 14.400000 14.400000 14.400000 14.377038 14.400000 14.377947 64: 14.400000 14.378370 14.400000 14.380439 14.400000 14.400000 14.400000 71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 78: 14.390431 14.400000 14.400000 14.400000 14.391064 14.400000 14.384912 85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.390113 14.400000 92: 14.400000 14.400000 14.400000 14.400000 14.388870 14.400000 14.400000 99: 14.400000 14.400000 14.386035 14.400000 14.384898 14.400000 14.400000 106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 155: 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14.400000 435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 449: 14.400000 14.360432 14.400000 14.400000 14.400000 14.400000 14.400000 456: 14.400000 14.400000 14.363710 14.400000 14.400000 14.400000 14.400000 463: 14.400000 14.400000 14.364299 14.400000 14.400000 14.400000 14.400000 470: 14.400000 14.400000 14.400000 14.363289 14.400000 14.400000 14.362208 477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 491: 14.400000 14.400000 14.400000 14.365678 14.400000 14.400000 14.400000 498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363289 14.400000 505: 14.400000 14.400000 14.400000 14.361522 14.400000 14.368098 14.400000 512: 14.400000 14.363976 14.400000 14.400000 14.370432 14.400000 14.400000 519: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363968 14.400000 526: 14.400000 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14.400000 14.400000 715: 14.400000 14.374692 14.400000 14.400000 14.400000 14.373031 14.375837 722: 14.400000 14.400000 14.370074 14.400000 14.380072 14.400000 14.400000 729: 14.400000 14.400000 14.375022 14.372158 14.400000 14.373856 14.380242 736: 14.400000 14.377974 14.400000 14.400000 14.380573 14.400000 14.400000 743: 14.400000 14.400000 14.400000 14.370484 14.372158 14.375910 14.400000 750: 14.381582 14.375912 14.400000 14.400000 14.379288 14.400000 14.373737 757: 14.400000 14.400000 14.400000 14.379729 14.382285 14.378584 14.400000 764: 14.382311 14.400000 14.400000 14.374409 14.371245 14.379232 14.373945 771: 14.400000 14.376341 14.400000 14.400000 14.377043 14.378486 14.374858 778: 14.382054 14.400000 14.383869 14.381636 14.377184 14.400000 14.400000 785: 14.400000 14.372636 14.400000 14.368456 14.383921 14.400000 14.400000 792: 14.383458 14.400000 14.400000 14.400000 14.400000 14.400000 14.381953 799: 14.400000 14.374858 14.373072 14.378348 14.379772 14.400000 14.378216 806: 14.378852 14.400000 14.400000 14.400000 14.380161 14.400000 14.400000 813: 14.384556 14.381516 14.400000 14.376255 14.400000 14.380120 14.400000 820: 14.400000 14.380472 14.379996 14.400000 14.373072 14.400000 14.373126 827: 14.379728 14.388089 14.378410 14.377743 14.383644 14.400000 14.400000 834: 14.381170 14.377592 14.376925 14.384404 14.383167 14.400000 14.382056 841: 14.400000 14.383692 14.400000 14.383013 14.384733 14.400000 14.400000 848: 14.400000 14.380633 14.400000 14.400000 14.400000 14.373808 14.381358 855: 14.400000 14.400000 14.383124 14.400000 14.400000 14.385360 14.376255 862: 14.373590 14.400000 14.383049 14.386052 14.382506 14.381131 14.383698 869: 14.384781 14.379968 14.383657 14.384709 14.377957 14.400000 14.380975 876: 14.400000 14.375227 14.400000 14.379017 14.378731 14.378357 14.376010 883: 14.373652 14.383370 14.383357 14.385444 14.385424 14.381819 14.384645 890: 14.379402 14.389897 14.380433 14.400000 14.383857 14.385410 14.384756 897: 14.379335 14.385835 14.400000 14.385091 14.374477 14.383079 14.383855 904: 14.380149 14.374722 14.383296 14.381983 14.376090 14.383810 14.378363 911: 14.387375 14.383245 14.378412 14.383393 14.382951 14.382465 14.382804 918: 14.384507 14.385472 14.385336 14.385820 14.384140 14.385028 14.385702 925: 14.383042 14.388214 14.388256 14.382050 14.381706 14.379795 14.381159 932: 14.381897 14.378803 14.384372 14.381369 14.386079 14.387357 14.385924 939: 14.382744 14.381612 14.381032 14.386745 14.385849 14.379042 14.385090 946: 14.400000 14.381764 14.381240 14.379650 14.385693 14.385693 14.386153 953: 14.384626 14.387791 14.385449 14.400000 14.385665 14.400000 14.379731 960: 14.380272 14.385409 14.385781 14.381733 14.382438 14.385533 14.380583 967: 14.386516 14.384573 14.400000 14.378382 14.384594 14.400000 14.386153 974: 14.382680 14.389375 14.386802 14.381707 14.379398 14.380377 14.386666 981: 14.387596 14.388630 14.387987 14.379180 14.386395 14.386595 14.400000 988: 14.385128 14.382720 14.381637 14.387158 14.381496 14.389287 14.386767 995: 14.382154 14.388300 14.384113 14.381877 14.390676 14.383198 14.387762 1002: 14.386642 14.388993 14.383485 14.387635 14.390869 14.381952 14.382376 1009: 14.381221 14.379752 14.400000 14.382249 14.378060 14.383886 14.382511 1016: 14.387091 14.386270 14.384482 14.387626 14.381697 14.387252 14.400000 1023: 14.378331 14.384910 14.381021 14.388566 14.400000 14.388325 14.387032 1030: 14.378428 14.387252 14.379752 14.400000 14.384558 14.384911 14.381221 1037: 14.378848 14.384694 14.382523 14.382981 source getTriangles = 0, nGtris = 1962, nGsegs = 5886, Ds = 0 0 destin getTriangles = 0, nGtris = 790, nGsegs = 2370, Ds = 0 0 In caps_outputObjects: 2 Analyses found 1 Bounds found testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m25.369s user 0m25.660s sys 0m0.484s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm passed (as expected) ============================================= + rm -rf source.vs destin.vs + expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm testingAIM/aimInitialize instance = 0 unitSys = m! testingAIM/aimInputs instance = 0 index = 1! testingAIM/aimInputs instance = 0 index = 2! testingAIM/aimInputs instance = 0 index = 3! testingAIM/aimInputs instance = 0 index = 4! testingAIM/aimOutputs instance = 0 index = 1! testingAIM/aimOutputs instance = 0 index = 2! testingAIM/aimOutputs instance = 0 index = 3! testingAIM/aimInitialize instance = 1 unitSys = (null)! testingAIM/aimInputs instance = 1 index = 1! testingAIM/aimInputs instance = 1 index = 2! testingAIM/aimInputs instance = 1 index = 3! testingAIM/aimInputs instance = 1 index = 4! testingAIM/aimOutputs instance = 1 index = 1! testingAIM/aimOutputs instance = 1 index = 2! testingAIM/aimOutputs instance = 1 index = 3! Intent = child APath = /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM1 UnitSys = (null) Exec = 2 Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0) Dirty = 3 testingAIM/aimUpdateState instance = 0! tess is NULL! testingAIM/aimPreAnalysis instance = 0! testingAIM/aimPreAnalysis aim_getBounds = 0 aim_newGeometry = 0! getDiscr = -303 meshRef = NULL testingAIM/aimExecute instance = 0! testingAIM/aimPostAnalysis instance = 0 restart = 0! testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0! aim_getDiscr 0 on Interface = -303 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! testingAIM/aimUpdateState instance = 1! tess is NULL! testingAIM/aimPreAnalysis instance = 1! testingAIM/aimPreAnalysis aim_getBounds = 0 aim_newGeometry = 0! mesh file = /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile symLink = 0 getDiscr = -303 testingAIM/aimExecute instance = 1! testingAIM/aimPostAnalysis instance = 1 restart = 0! testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0! aim_getDiscr 1 on Interface = -303 *** testingAIMout (child) = 12.340000 1 1 *** testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m4.249s user 0m4.086s sys 0m0.557s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm passed (as expected) ============================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.8/CAPS/unit/DARWIN64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.8,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys #200'. [Checks API] No suitable checks publisher found. [PostBuildScript] - [INFO] Executing post build scripts. [PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX [WS-CLEANUP] Deleting project workspace... [WS-CLEANUP] done Finished: SUCCESS