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Full LogEGADS : 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= 88 142 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= 310 542 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= 1738 3468 512 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1738 3468 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= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 315 552 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 315 552 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= 1739 3470 512 OVERALL : CPU Time = 0.046 seconds Body 1 (of 2) Number of nodes = 519 Number of elements = 1034 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1034 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1220 Number of elements = 2436 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2436 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1739 Total number of elements = 3470 .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 7.7.0 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 Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 5 6 -7 -1 EGADS : 3 Yes 1 -2 7 9 -8 EGADS : 4 Yes 1 -10 3 8 -11 EGADS : 5 Yes 1 4 10 -12 -5 EGADS : 6 Yes 1 -6 12 11 -9 EGADS : 7 Yes 1 -13 14 15 -16 EGADS : 8 Yes 1 -17 18 13 -19 EGADS : 9 Yes 1 20 22 -21 -14 EGADS : 10 Yes 1 -15 23 17 -24 EGADS : 11 Yes 1 16 24 19 EGADS : 12 Yes 1 25 26 -20 -18 EGADS : 13 Yes 1 21 27 -25 -23 EGADS : 14 Yes 1 -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= 17055 33380 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= 17164 33598 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= 137 232 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= 137 232 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= 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 = 0.871 seconds Body 1 (of 1) Number of nodes = 37391 Number of elements = 74774 Number of node elements = 0 Number of line elements = 0 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 7.7.0 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 Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 5 6 -7 -1 EGADS : 3 Yes 1 -2 7 9 -8 EGADS : 4 Yes 1 -10 3 8 -11 EGADS : 5 Yes 1 4 10 -12 -5 EGADS : 6 Yes 1 -6 12 11 -9 EGADS : 7 Yes 1 -13 14 15 -16 EGADS : 8 Yes 1 -17 18 13 -19 EGADS : 9 Yes 1 20 22 -21 -14 EGADS : 10 Yes 1 -15 23 17 -24 EGADS : 11 Yes 1 16 24 19 EGADS : 12 Yes 1 25 26 -20 -18 EGADS : 13 Yes 1 21 27 -25 -23 EGADS : 14 Yes 1 -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 = 5.65685 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.62074 AFLR4 : Abs Min Surf Spacing = 0.0141421 AFLR4 : Min Surf Spacing = 0.0282843 AFLR4 : Max Surf Spacing = 0.565685 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= 6411 12401 0 AFLR4 : Nodes, Trias,Quads= 3253 6085 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= 6519 12617 0 AFLR4 : Nodes, Trias,Quads= 3180 5939 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5814 11207 0 AFLR4 : Nodes, Trias,Quads= 3048 5675 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 257 412 0 AFLR4 : Nodes, Trias,Quads= 256 410 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= 5862 11303 0 AFLR4 : Nodes, Trias,Quads= 3028 5635 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 258 414 0 AFLR4 : Nodes, Trias,Quads= 256 410 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 12856 25704 2334 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 12856 25704 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 137 232 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= 137 232 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= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6200 11975 0 AFLR4 : Nodes, Trias,Quads= 4633 8841 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= 6154 11884 0 AFLR4 : Nodes, Trias,Quads= 4634 8844 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5942 11461 0 AFLR4 : Nodes, Trias,Quads= 4482 8541 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 263 424 0 AFLR4 : Nodes, Trias,Quads= 268 434 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 226 328 0 AFLR4 : Nodes, Trias,Quads= 122 120 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5975 11528 0 AFLR4 : Nodes, Trias,Quads= 4473 8524 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 265 428 0 AFLR4 : Nodes, Trias,Quads= 270 438 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 18601 37194 2370 OVERALL : CPU Time = 0.395 seconds Body 1 (of 1) Number of nodes = 18601 Number of elements = 37194 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 37194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 18601 Total number of elements = 37194 .. 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 7.7.0 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 Sense Edges EGADS : 1 Yes 1 -1 -2 3 4 EGADS : 2 Yes 1 -5 -4 6 2 EGADS : 3 Yes 1 7 8 -9 -10 EGADS : 4 Yes 1 -11 14 13 -12 EGADS : 5 Yes 1 15 11 -16 -7 EGADS : 6 Yes 1 -17 9 18 -13 EGADS : 7 Yes 1 10 17 -14 -15 EGADS : 8 Yes 1 -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= 88 142 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= 310 542 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= 1591 3174 432 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1591 3174 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= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 315 552 0 AFLR4 : Nodes, Trias,Quads= 308 538 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= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 315 552 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= 1593 3178 428 OVERALL : CPU Time = 0.047 seconds Body 1 (of 2) Number of nodes = 373 Number of elements = 742 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 742 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1220 Number of elements = 2436 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2436 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1593 Total number of elements = 3178 . 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 7.7.0 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 Sense Edges EGADS : 1 Yes 1 -1 2 1 -2 EGADS : 2 Yes 1 3 4 -5 -6 EGADS : 3 Yes 1 -7 10 9 -8 EGADS : 4 Yes 1 11 7 -12 -3 EGADS : 5 Yes 1 -13 5 14 -9 EGADS : 6 Yes 1 6 13 -10 -11 EGADS : 7 Yes 1 -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= 88 142 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= 311 544 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= 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= 1831 3658 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1831 3658 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= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 315 552 0 AFLR4 : Nodes, Trias,Quads= 308 538 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= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 315 552 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= 1883 3762 496 OVERALL : CPU Time = 0.066 seconds Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 (of 2) Number of nodes = 663 Number of elements = 1326 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1326 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1220 Number of elements = 2436 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2436 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1883 Total number of elements = 3762 .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 = 1 Number of node elements = 1 Number of line 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 44 ---------------------------- Total number of nodes = 47 Total number of elements = 45 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 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) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Body 1 (of 1) Number of nodes = 25 Number of elements = 16 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 0 Number of quadrilateral elements = 16 ---------------------------- Total number of nodes = 25 Total number of elements = 16 Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 1 Name = plateEdge, index = 1 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 1 Name = plate, index = 1 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsResponse attributes ................ Number of unique capsResponse attributes = 0 Mapping 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 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 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 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 = 9573 Number of elements = 19142 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19142 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6160 Number of elements = 12316 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 12316 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 104 Number of elements = 204 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 204 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15837 Total number of elements = 31662 .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 = 9583 Number of elements = 19158 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19158 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9583 Total number of elements = 19158 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) 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) 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1700DB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1700DB000 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 8) Number of nodes = 873 Number of elements = 1742 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1742 Number of quadrilateral elements = 0 Body 3 (of 8) Number of nodes = 1315 Number of elements = 2626 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2626 Number of quadrilateral elements = 0 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 4 (of 8) Number of nodes = 2048 Number of elements = 4096 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 5 (of 8) Number of nodes = 822 Number of elements = 1640 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1640 Number of quadrilateral elements = 0 Body 6 (of 8) Number of nodes = 1959 Number of elements = 3918 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3918 Number of quadrilateral elements = 0 Body 7 (of 8) Number of nodes = 935 Number of elements = 1866 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1866 Number of quadrilateral elements = 0 Body 8 (of 8) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 83220 Total number of elements = 166416 . 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 node elements = 0 Number of line elements = 0 Number of triangle elements = 3072 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 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) 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1700DB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1700DB000 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 = 1959 Number of elements = 3918 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3918 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75689 Total number of elements = 151374 . 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 = 935 Number of elements = 1866 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1866 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74665 Total number of elements = 149322 . 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 = 1315 Number of elements = 2626 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2626 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 75045 Total number of elements = 150082 . 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 = 873 Number of elements = 1742 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1742 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74603 Total number of elements = 149198 .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 = 9583 Number of elements = 19158 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19158 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9583 Total number of elements = 19158 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 = 7151 Number of elements = 14294 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 14294 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7151 Total number of elements = 14294 .. 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 = 822 Number of elements = 1640 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1640 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 147456 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 74552 Total number of elements = 149096 . 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) Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Body 1 (of 2) Number of nodes = 2048 Number of elements = 4096 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 4096 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 73730 Number of elements = 147456 Number of node elements = 0 Number of line elements = 0 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 = 7800 Number of elements = 15596 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15596 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5906 Number of elements = 11808 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11808 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 542 Number of elements = 1080 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1080 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14248 Total number of elements = 28484 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 - 14248, elements - 28484 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.105876 Creating surface mesh ... Surface mesh seconds: 0.020636 Recovering boundaries... Boundary recovery seconds: 0.10537 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.030506 Recovering Delaunayness... Delaunay recovery seconds: 0.047986 Refining mesh... 18992 insertions, added 13405 points, 688228 tetrahedra in queue. 6324 insertions, added 2619 points, 589108 tetrahedra in queue. 8430 insertions, added 2014 points, 124223 tetrahedra in queue. Refinement seconds: 1.73515 Smoothing vertices... Mesh smoothing seconds: 1.51917 Improving mesh... Mesh improvement seconds: 0.044091 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.018067 Total running seconds: 3.62717 Statistics: Input points: 14248 Input facets: 28484 Input segments: 42726 Input holes: 2 Input regions: 0 Mesh points: 33028 Mesh tetrahedra: 159264 Mesh faces: 332770 Mesh faces on exterior boundary: 28484 Mesh faces on input facets: 28484 Mesh edges on input segments: 42726 Steiner points inside domain: 18780 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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml ..... Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream Error: Python error occurred while writing namelist file self._update_tokens() File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read return parser.read(nml_path) ^^^^^^^^^^^^^^^^^^^^^ File "/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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 = 4048 Number of elements = 6648 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5204 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 = 7800 Number of elements = 15596 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15596 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5906 Number of elements = 11808 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11808 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 542 Number of elements = 1080 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1080 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14248 Total number of elements = 28484 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 - 14248, elements - 28484 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.101698 Creating surface mesh ... Surface mesh seconds: 0.018645 Recovering boundaries... Boundary recovery seconds: 0.094846 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.029991 Recovering Delaunayness... Delaunay recovery seconds: 0.043824 Refining mesh... 18992 insertions, added 13405 points, 688228 tetrahedra in queue. 6324 insertions, added 2619 points, 589108 tetrahedra in queue. 8430 insertions, added 2014 points, 124223 tetrahedra in queue. Refinement seconds: 1.56761 Smoothing vertices... Mesh smoothing seconds: 1.47458 Improving mesh... Mesh improvement seconds: 0.039348 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.006884 Total running seconds: 3.37777 Statistics: Input points: 14248 Input facets: 28484 Input segments: 42726 Input holes: 2 Input regions: 0 Mesh points: 33028 Mesh tetrahedra: 159264 Mesh faces: 332770 Mesh faces on exterior boundary: 28484 Mesh faces on input facets: 28484 Mesh edges on input segments: 42726 Steiner points inside domain: 18780 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 (8.0.0) " 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 (8.0.0) " . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... Running xFoil...... . ---------------------------------------------------------------------- Ran 67 tests in 47.301s 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 0m0.147s user 0m0.075s sys 0m0.007s ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest + /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.127s user 0m0.069s sys 0m0.005s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest + /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest vlmUtils Tests passed! real 0m0.130s user 0m0.075s sys 0m0.006s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest passed (as expected) ============================================= + rm -rf aimTest + expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm' + /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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 = 2006! testingAIM/aimDiscr: npts = 1062! testingAIM/aimDiscr: tname = Interface, instance = 0! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 6 matches Interface! testingAIM/aimDiscr: ntris = 772! testingAIM/aimDiscr: npts = 433! testingAIM/aimTransfer name = scalar instance = 0 npts = 433/1! CAPS Info: Bound 'Interface' Normalized Integrated 'scalar' Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.969212e-09 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds ParamName has type VALUE, subtype PARAMETER with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 2 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 2 value = 0.000000 (null) Param has type VALUE, subtype PARAMETER with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 3 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 3 value = 99 (null) num has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 6 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 6 value = 8.000000 (null) x has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 7 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 value (1x3) = 1: Entry1 -> Value1 2: Entry2 -> Value2 3: Entry3 -> Value3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 8 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs 1 Bodies, 1 Tessellations testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 12 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 12 value (1x3) = 1: Entry1 -> newValue1 2: Entry2 -> newValue2 3: Entry3 -> newValue3 tessIn has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 13 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 10 value (0x0) = NULL with len = 0 meter testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 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 VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 6000002ec000 value = 6000002ec000 ego lazy: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 14 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 1062 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 1062 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 26 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 15 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:59:07 26 1062 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 433 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 23 433 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 25 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:54 25 433 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:74258 jenkins 2024/03/28 22:58:53 0 testingAIM/aimTransfer name = vector instance = 0 npts = 433/3! 433 points, rank=3, units=(null) 1: 14.400001 14.400001 14.400000 14.400001 14.400001 14.400000 14.400000 8: 14.400001 14.400000 14.400003 14.380571 14.400001 14.381441 14.400000 15: 14.400000 14.400002 14.400002 14.400000 14.400000 14.400002 14.400000 22: 14.400001 14.400001 14.400000 14.383000 14.400000 14.400000 14.400001 29: 14.400000 14.390397 14.400001 14.400000 14.400000 14.400002 14.400002 36: 14.400001 14.400001 14.390256 14.400001 14.389522 14.400002 14.400002 43: 14.400002 14.400000 14.400000 14.400002 14.400003 14.400003 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14.400001 14.400002 14.400001 14.400002 14.400001 14.400002 148: 14.399999 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001 155: 14.400001 14.400001 14.400001 14.400003 14.400001 14.400001 14.400001 162: 14.400001 14.400001 14.400002 14.400001 14.400001 14.400000 14.400001 169: 14.400001 14.400001 14.400001 14.400000 14.400001 14.400001 14.400002 176: 14.400000 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002 183: 14.400001 14.400002 14.400002 14.400001 14.400001 14.400002 14.400001 190: 14.400001 14.400001 14.400002 14.399999 14.400001 14.400002 14.400002 197: 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001 14.400001 204: 14.400002 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002 211: 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001 218: 14.400000 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001 225: 14.400001 14.400001 14.400002 14.400002 14.400002 14.400001 14.400001 232: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400000 239: 14.400000 14.400002 14.400000 14.400001 14.400001 14.400001 14.400002 246: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 253: 14.400002 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001 260: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 267: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001 274: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400002 281: 14.400001 14.400001 14.400000 14.400001 14.399999 14.400001 14.400002 288: 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 295: 14.400003 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001 302: 14.400002 14.400001 14.400001 14.400000 14.400001 14.400002 14.400000 309: 14.400002 14.400001 14.400001 14.400001 14.400002 14.400001 14.400000 316: 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001 14.399999 323: 14.400001 14.400001 14.355208 14.400002 14.400002 14.400001 14.400001 330: 14.400000 14.400000 14.400001 14.399999 14.400001 14.400000 14.400001 337: 14.400001 14.400001 14.400003 14.400002 14.399999 14.400001 14.400000 344: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 351: 14.400002 14.400001 14.400000 14.400006 14.400002 14.400001 14.400000 358: 14.400000 14.400001 14.400001 14.400001 14.399999 14.400002 14.400001 365: 14.400001 14.400002 14.400000 14.400001 14.357384 14.400000 14.399999 372: 14.400002 14.400002 14.400002 14.400001 14.400001 14.400001 14.399999 379: 14.400001 14.399999 14.400002 14.400002 14.400001 14.400001 14.400001 386: 14.400002 14.400000 14.399999 14.400001 14.400001 14.400000 14.400000 393: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001 400: 14.400002 14.400001 14.399999 14.400002 14.399999 14.400001 14.400001 407: 14.400000 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001 414: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400004 14.359138 421: 14.400005 14.399999 14.400001 14.400000 14.400001 14.400001 14.400001 428: 14.400002 14.399999 14.400000 14.400000 14.400002 14.400001 14.400004 435: 14.400004 14.362514 14.362329 14.400001 14.399999 14.400001 14.400001 442: 14.400001 14.400001 14.400002 14.400003 14.399999 14.400001 14.400002 449: 14.400001 14.400001 14.400002 14.400001 14.399999 14.400001 14.399999 456: 14.400001 14.400002 14.400004 14.400000 14.399999 14.400000 14.400000 463: 14.400001 14.399999 14.362644 14.400001 14.400002 14.399999 14.399999 470: 14.400001 14.400001 14.400001 14.399999 14.400001 14.400001 14.366558 477: 14.400001 14.400006 14.400001 14.400000 14.400001 14.400000 14.400001 484: 14.400004 14.400001 14.400005 14.399999 14.400002 14.400001 14.400005 491: 14.399999 14.400002 14.399999 14.367443 14.400003 14.400001 14.400000 498: 14.400001 14.400001 14.362493 14.399999 14.400001 14.399999 14.400001 505: 14.399999 14.400005 14.399999 14.400004 14.400001 14.400004 14.363391 512: 14.400001 14.366127 14.400002 14.400004 14.399999 14.400001 14.400004 519: 14.399999 14.400001 14.399999 14.400001 14.364370 14.399999 14.400005 526: 14.400005 14.365691 14.399999 14.369927 14.400002 14.400001 14.400000 533: 14.400000 14.368701 14.400001 14.399999 14.400000 14.399999 14.364370 540: 14.360914 14.399999 14.400001 14.400005 14.400004 14.400002 14.399999 547: 14.400000 14.399999 14.366320 14.400001 14.400003 14.370716 14.367841 554: 14.367007 14.367819 14.399999 14.369566 14.400001 14.399999 14.399999 561: 14.366648 14.367456 14.400005 14.400002 14.366344 14.400000 14.369947 568: 14.400004 14.400004 14.367007 14.373369 14.400001 14.400000 14.400002 575: 14.365408 14.400004 14.400000 14.400004 14.399999 14.400005 14.400002 582: 14.399999 14.400002 14.400001 14.400004 14.400004 14.369590 14.400004 589: 14.372211 14.400002 14.400000 14.400002 14.400002 14.400003 14.400000 596: 14.400004 14.400004 14.373403 14.368774 14.400000 14.400000 14.399999 603: 14.400001 14.400002 14.370406 14.367007 14.400001 14.372363 14.400001 610: 14.370598 14.400000 14.399999 14.400002 14.400004 14.372320 14.400000 617: 14.400000 14.368054 14.400004 14.400000 14.378759 14.400000 14.366320 624: 14.400000 14.400000 14.400004 14.370366 14.370760 14.400002 14.400004 631: 14.400004 14.400004 14.369692 14.365169 14.400004 14.400004 14.400000 638: 14.399999 14.400005 14.368369 14.400001 14.400000 14.400000 14.400003 645: 14.400003 14.399999 14.400002 14.400001 14.370996 14.400001 14.400002 652: 14.400002 14.367680 14.400000 14.400004 14.400000 14.400003 14.400003 659: 14.367301 14.400000 14.371052 14.400000 14.400004 14.375426 14.372158 666: 14.400000 14.370146 14.399999 14.400004 14.399999 14.368248 14.400000 673: 14.400003 14.369989 14.370548 14.368054 14.377207 14.400000 14.369613 680: 14.368333 14.400004 14.400001 14.377741 14.400003 14.400000 14.400004 687: 14.400003 14.400003 14.400000 14.377967 14.399999 14.376780 14.370538 694: 14.373367 14.400000 14.400003 14.400004 14.370294 14.371052 14.400000 701: 14.400003 14.370426 14.400004 14.400001 14.400001 14.376281 14.375920 708: 14.377357 14.400000 14.376914 14.400001 14.400002 14.400002 14.400002 715: 14.400003 14.379840 14.370996 14.400003 14.400003 14.370673 14.400000 722: 14.363653 14.362250 14.373534 14.400003 14.379510 14.400000 14.374657 729: 14.400003 14.400004 14.400002 14.379679 14.400000 14.379827 14.372479 736: 14.400002 14.380745 14.379344 14.379423 14.400003 14.380718 14.372490 743: 14.376209 14.400000 14.400000 14.400000 14.400000 14.400000 14.400003 750: 14.375014 14.373465 14.400000 14.400003 14.380638 14.400002 14.400002 757: 14.400000 14.376150 14.400003 14.400003 14.370382 14.379062 14.379044 764: 14.382714 14.371636 14.380688 14.372490 14.400004 14.380301 14.400003 771: 14.400003 14.400003 14.400003 14.381338 14.400003 14.400000 14.375566 778: 14.383460 14.400000 14.400000 14.382573 14.378742 14.378784 14.400002 785: 14.400003 14.377962 14.400003 14.388515 14.372960 14.400003 14.373659 792: 14.400000 14.376226 14.400000 14.400000 14.373627 14.400000 14.400002 799: 14.379592 14.400001 14.384129 14.381281 14.380925 14.400002 14.400000 806: 14.376874 14.400003 14.400000 14.376488 14.400002 14.372785 14.382064 813: 14.400002 14.400002 14.400002 14.400002 14.400002 14.400003 14.400003 820: 14.375490 14.374772 14.400003 14.375179 14.376681 14.379475 14.400003 827: 14.374392 14.379479 14.377005 14.387430 14.400002 14.382223 14.400003 834: 14.374371 14.383997 14.382259 14.386520 14.400000 14.400002 14.384358 841: 14.381380 14.373136 14.380004 14.382103 14.400002 14.400000 14.376043 848: 14.400000 14.381875 14.400002 14.377417 14.379456 14.400000 14.379534 855: 14.400002 14.400003 14.400000 14.400003 14.400000 14.400000 14.382400 862: 14.384944 14.376706 14.383227 14.400002 14.380291 14.400002 14.382257 869: 14.400003 14.384774 14.384820 14.382273 14.373450 14.400000 14.400003 876: 14.375908 14.378550 14.400000 14.377290 14.382472 14.379168 14.383016 883: 14.385491 14.382723 14.400003 14.400002 14.378971 14.385404 14.380466 890: 14.384576 14.400003 14.377221 14.400000 14.381355 14.383645 14.384247 897: 14.385287 14.383280 14.375114 14.400002 14.400000 14.400000 14.400000 904: 14.382426 14.382735 14.400002 14.382499 14.387660 14.382883 14.400002 911: 14.383520 14.387020 14.383842 14.382243 14.400000 14.378098 14.383884 918: 14.383573 14.384907 14.386099 14.400002 14.383499 14.385888 14.400002 925: 14.377060 14.378436 14.381620 14.380706 14.400000 14.373575 14.383742 932: 14.381255 14.382997 14.384659 14.382920 14.400000 14.400002 14.377577 939: 14.400000 14.386915 14.386123 14.384593 14.381816 14.381745 14.385286 946: 14.385286 14.382005 14.385759 14.385133 14.388988 14.381642 14.387570 953: 14.386633 14.386532 14.381505 14.386235 14.385447 14.400000 14.380013 960: 14.400000 14.382953 14.400002 14.383380 14.385229 14.383810 14.382999 967: 14.385309 14.400002 14.400002 14.382711 14.383198 14.385759 14.387667 974: 14.385183 14.384109 14.387476 14.400002 14.384433 14.388306 14.400002 981: 14.400002 14.383798 14.386396 14.386806 14.383774 14.389577 14.400000 988: 14.379854 14.381554 14.377995 14.375728 14.378018 14.382139 14.386343 995: 14.386055 14.378954 14.383869 14.400002 14.383263 14.385113 14.381831 1002: 14.400002 14.386892 14.388833 14.386742 14.385055 14.385000 14.381934 1009: 14.381408 14.380687 14.379175 14.380043 14.381323 14.375969 14.381364 1016: 14.384193 14.380959 14.400002 14.400002 14.400002 14.385962 14.400002 1023: 14.386889 14.381389 14.400002 14.379351 14.387189 14.400000 14.382624 1030: 14.400002 14.387047 14.400002 14.386889 14.379175 14.377388 14.389345 1037: 14.400002 14.400000 14.400000 14.381891 14.380687 14.400002 14.400000 1044: 14.383688 14.400002 14.400002 14.400002 14.383791 14.400000 14.400002 1051: 14.400003 14.400000 14.376605 14.400002 14.400000 14.376130 14.400003 1058: 14.383633 14.400002 14.400000 14.378191 14.384880 source getTriangles = 0, nGtris = 2006, nGsegs = 6018, Ds = 0 0 destin getTriangles = 0, nGtris = 772, nGsegs = 2316, Ds = 0 0 In caps_outputObjects: 2 Analyses found 1 Bounds found testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m14.023s user 0m13.605s sys 0m0.220s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm passed (as expected) ============================================= + rm -rf source.vs destin.vs + expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm' + /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/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 0m0.562s user 0m0.382s sys 0m0.132s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected) ============================================= ++ set +x [Execution node] check if [viggen] is in [[windows10x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [GNU C Compiler (gcc)] Successfully parsed console log [GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates) [GNU C Compiler (gcc)] Skipping post processing [GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues [GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN_ARM64') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #626'. [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