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Full LogEGADS : 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 = 0.054 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 1.24 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 = 1.445 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 1.24 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 = 0.650 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 1.24 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= 199 366 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= 1592 3176 428 OVERALL : CPU Time = 0.049 seconds Body 1 (of 2) Number of nodes = 372 Number of elements = 740 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 740 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 = 1592 Total number of elements = 3176 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.24 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 = 0.086 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 = 120 Number of elements = 236 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 236 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15853 Total number of elements = 31694 .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:60313) 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) 1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 17355B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 17355B000 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) 1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1DACB5000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 17355B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 17355B000 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 = 7137 Number of elements = 14266 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 14266 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7137 Total number of elements = 14266 . 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 = 7802 Number of elements = 15600 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15600 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 = 545 Number of elements = 1086 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1086 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14253 Total number of elements = 28494 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 - 14253, elements - 28494 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.258308 Creating surface mesh ... Surface mesh seconds: 0.044405 Recovering boundaries... Boundary recovery seconds: 0.17169 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.063925 Recovering Delaunayness... Delaunay recovery seconds: 0.089215 Refining mesh... 18999 insertions, added 13806 points, 712098 tetrahedra in queue. 6326 insertions, added 2564 points, 586841 tetrahedra in queue. 8433 insertions, added 1779 points, 64950 tetrahedra in queue. Refinement seconds: 3.50194 Smoothing vertices... Mesh smoothing seconds: 3.23226 Improving mesh... Mesh improvement seconds: 0.1314 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.024654 Total running seconds: 7.51853 Statistics: Input points: 14253 Input facets: 28494 Input segments: 42741 Input holes: 2 Input regions: 0 Mesh points: 33071 Mesh tetrahedra: 159280 Mesh faces: 332807 Mesh faces on exterior boundary: 28494 Mesh faces on input facets: 28494 Mesh edges on input segments: 42741 Steiner points inside domain: 18818 Done meshing using TetGen! Analysis object with the name, fun3dAIM, has already been initilized An altName of fun3dAIM_1 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/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_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml ..... Error: Python error occurred while writing namelist file Traceback (most recent call last): File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/venv/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream self._update_tokens() File "/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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 = 7802 Number of elements = 15600 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15600 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 = 545 Number of elements = 1086 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1086 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14253 Total number of elements = 28494 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 - 14253, elements - 28494 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.259874 Creating surface mesh ... Surface mesh seconds: 0.041723 Recovering boundaries... Boundary recovery seconds: 0.161573 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.061745 Recovering Delaunayness... Delaunay recovery seconds: 0.089393 Refining mesh... 18999 insertions, added 13806 points, 712098 tetrahedra in queue. 6326 insertions, added 2564 points, 586841 tetrahedra in queue. 8433 insertions, added 1779 points, 64950 tetrahedra in queue. Refinement seconds: 3.45817 Smoothing vertices... Mesh smoothing seconds: 3.14577 Improving mesh... Mesh improvement seconds: 0.132983 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.023417 Total running seconds: 7.37547 Statistics: Input points: 14253 Input facets: 28494 Input segments: 42741 Input holes: 2 Input regions: 0 Mesh points: 33071 Mesh tetrahedra: 159280 Mesh faces: 332807 Mesh faces on exterior boundary: 28494 Mesh faces on input facets: 28494 Mesh edges on input segments: 42741 Steiner points inside domain: 18818 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 116.849s 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 0m0.142s user 0m0.071s sys 0m0.018s ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/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 0m0.129s user 0m0.068s sys 0m0.011s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest vlmUtils Tests passed! real 0m0.130s user 0m0.068s sys 0m0.014s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest passed (as expected) ============================================= + rm -rf aimTest + expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm Root Path = /Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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 = 1986! testingAIM/aimDiscr: npts = 1052! testingAIM/aimDiscr: tname = Interface, instance = 0! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 6 matches Interface! testingAIM/aimDiscr: ntris = 794! testingAIM/aimDiscr: npts = 444! testingAIM/aimTransfer name = scalar instance = 0 npts = 444/1! CAPS Info: Bound 'Interface' Normalized Integrated 'scalar' Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.563194e-13 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:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 2 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 2 value = 0.000000 (null) Param has type VALUE, subtype PARAMETER with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 3 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 3 value = 99 (null) num has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 6 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 6 value = 8.000000 (null) x has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 7 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 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:50241 jenkins 2023/12/25 17:59:14 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:14 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 8 value (0x0) = NULL with len = 0 writer testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:24 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 18 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:24 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 28 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 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:50241 jenkins 2023/12/25 17:59:14 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 12 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:15 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 13 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 10 value (0x0) = NULL with len = 0 writer testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 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:50241 jenkins 2023/12/25 17:59:24 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 600001df0640 value = 600001df0640 ego lazy: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:24 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:24 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 28 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 14 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 1052 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 1052 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 26 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 15 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:23 26 1052 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 444 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 23 444 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 25 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:15 25 444 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:50241 jenkins 2023/12/25 17:59:14 0 testingAIM/aimTransfer name = vector instance = 0 npts = 444/3! 444 points, rank=3, units=(null) 1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 8: 14.400000 14.400000 14.400000 14.378831 14.400000 14.400000 14.400000 15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 22: 14.400000 14.400000 14.400000 14.383512 14.400000 14.400000 14.400000 29: 14.400000 14.390686 14.400000 14.400000 14.400000 14.400000 14.400000 36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 57: 14.400000 14.400000 14.400000 14.400000 14.377096 14.400000 14.378002 64: 14.400000 14.378425 14.400000 14.380488 14.400000 14.400000 14.400000 71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 78: 14.400000 14.386209 14.400000 14.400000 14.400000 14.400000 14.384098 85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 92: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 99: 14.400000 14.400000 14.386071 14.400000 14.384936 14.400000 14.400000 106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 260: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 337: 14.400000 14.400000 14.400000 14.400000 14.356558 14.400000 14.400000 344: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 379: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 386: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 414: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 421: 14.400000 14.364389 14.400000 14.400000 14.400000 14.400000 14.400000 428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 449: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 456: 14.400000 14.400000 14.361360 14.400000 14.400000 14.400000 14.400000 463: 14.400000 14.361740 14.400000 14.400000 14.400000 14.400000 14.361165 470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.360532 484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 491: 14.363802 14.400000 14.400000 14.361619 14.400000 14.368179 14.400000 498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 505: 14.400000 14.400000 14.362304 14.400000 14.400000 14.400000 14.400000 512: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 519: 14.400000 14.400000 14.373001 14.400000 14.400000 14.365765 14.400000 526: 14.364059 14.360074 14.400000 14.400000 14.364067 14.400000 14.366792 533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 540: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 547: 14.400000 14.366792 14.400000 14.365283 14.370506 14.400000 14.400000 554: 14.400000 14.368606 14.400000 14.400000 14.400000 14.400000 14.400000 561: 14.400000 14.400000 14.400000 14.400000 14.366173 14.400000 14.400000 568: 14.400000 14.400000 14.400000 14.400000 14.368001 14.400000 14.400000 575: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 582: 14.400000 14.369112 14.400000 14.400000 14.371298 14.400000 14.368001 589: 14.400000 14.400000 14.372161 14.400000 14.400000 14.368488 14.400000 596: 14.400000 14.367602 14.400000 14.400000 14.400000 14.400000 14.400000 603: 14.400000 14.400000 14.400000 14.368001 14.366391 14.400000 14.400000 610: 14.371426 14.400000 14.400000 14.369447 14.400000 14.400000 14.400000 617: 14.400000 14.400000 14.400000 14.377309 14.400000 14.400000 14.400000 624: 14.368789 14.400000 14.400000 14.400000 14.370365 14.400000 14.367429 631: 14.400000 14.368910 14.400000 14.373079 14.400000 14.400000 14.400000 638: 14.400000 14.400000 14.400000 14.400000 14.400000 14.377329 14.400000 645: 14.376154 14.400000 14.400000 14.367922 14.400000 14.373272 14.400000 652: 14.378235 14.400000 14.400000 14.400000 14.400000 14.366804 14.400000 659: 14.368813 14.400000 14.377324 14.372228 14.400000 14.373478 14.375283 666: 14.400000 14.378016 14.400000 14.400000 14.371143 14.400000 14.372419 673: 14.400000 14.376808 14.400000 14.400000 14.400000 14.400000 14.400000 680: 14.400000 14.377703 14.400000 14.379051 14.372699 14.379817 14.400000 687: 14.400000 14.400000 14.400000 14.377610 14.375648 14.400000 14.400000 694: 14.369238 14.400000 14.369944 14.400000 14.371318 14.400000 14.375746 701: 14.375803 14.400000 14.400000 14.400000 14.400000 14.400000 14.372846 708: 14.400000 14.372368 14.378170 14.400000 14.374755 14.378030 14.400000 715: 14.400000 14.400000 14.374706 14.400000 14.400000 14.371318 14.400000 722: 14.375898 14.400000 14.370149 14.400000 14.400000 14.374805 14.377143 729: 14.373864 14.400000 14.379637 14.400000 14.400000 14.382610 14.379415 736: 14.400000 14.379571 14.381325 14.400000 14.373140 14.378638 14.400000 743: 14.400000 14.400000 14.370559 14.400000 14.375085 14.372229 14.372229 750: 14.400000 14.382920 14.375972 14.400000 14.374657 14.381204 14.371275 757: 14.379781 14.374921 14.400000 14.380608 14.382356 14.374971 14.400000 764: 14.400000 14.378465 14.400000 14.400000 14.400000 14.400000 14.400000 771: 14.400000 14.400000 14.400000 14.375852 14.383099 14.373140 14.373018 778: 14.400000 14.382099 14.382909 14.400000 14.379692 14.400000 14.400000 785: 14.384926 14.400000 14.388861 14.400000 14.400000 14.383987 14.383981 792: 14.400000 14.375970 14.400000 14.370583 14.381998 14.400000 14.400000 799: 14.400000 14.383910 14.400000 14.378728 14.388120 14.378271 14.400000 806: 14.375163 14.375173 14.400000 14.370338 14.382454 14.379061 14.380211 813: 14.384486 14.378136 14.400000 14.383500 14.381847 14.382863 14.400000 820: 14.400000 14.377101 14.375595 14.400000 14.373292 14.379779 14.380376 827: 14.400000 14.373874 14.400000 14.383686 14.380422 14.400000 14.400000 834: 14.383166 14.379052 14.383605 14.380344 14.400000 14.400000 14.382794 841: 14.375125 14.400000 14.382029 14.383056 14.400000 14.400000 14.378276 848: 14.400000 14.381153 14.400000 14.375008 14.377799 14.374541 14.381405 855: 14.374929 14.400000 14.400000 14.381218 14.379742 14.383231 14.400000 862: 14.381834 14.384969 14.384922 14.375179 14.400000 14.381622 14.379954 869: 14.383733 14.378833 14.400000 14.382551 14.400000 14.376921 14.374541 876: 14.400000 14.400000 14.400000 14.400000 14.400000 14.373804 14.376151 883: 14.400000 14.400000 14.385119 14.400000 14.384771 14.385277 14.400000 890: 14.384683 14.400000 14.383245 14.384658 14.385167 14.384820 14.400000 897: 14.381917 14.384748 14.381022 14.384180 14.376570 14.400000 14.376181 904: 14.400000 14.382409 14.383895 14.377432 14.376314 14.385461 14.385212 911: 14.383287 14.381870 14.382994 14.385890 14.385447 14.386114 14.385828 918: 14.385723 14.385871 14.400000 14.383085 14.400000 14.381737 14.383942 925: 14.384917 14.400000 14.381285 14.382095 14.400000 14.400000 14.376314 932: 14.376070 14.400000 14.382758 14.379454 14.378857 14.383739 14.386359 939: 14.380880 14.379472 14.380483 14.384546 14.387537 14.382787 14.385066 946: 14.400000 14.378835 14.386778 14.383010 14.383809 14.381921 14.386550 953: 14.378436 14.400000 14.381287 14.400000 14.385729 14.382203 14.400000 960: 14.400000 14.381514 14.400000 14.385837 14.383749 14.385373 14.381900 967: 14.400000 14.387191 14.381810 14.384633 14.386224 14.386188 14.382724 974: 14.384664 14.388330 14.386817 14.400000 14.400000 14.400000 14.380427 981: 14.387139 14.400000 14.387627 14.379233 14.389580 14.382421 14.378624 988: 14.380128 14.382483 14.383381 14.385844 14.382032 14.378711 14.381543 995: 14.389314 14.386279 14.381344 14.400000 14.386188 14.386800 14.386835 1002: 14.387324 14.384153 14.382603 14.386700 14.386676 14.386861 14.389231 1009: 14.384737 14.378482 14.379803 14.381706 14.400000 14.400000 14.378115 1016: 14.380762 14.381783 14.383927 14.382199 14.385896 14.386358 14.379724 1023: 14.385043 14.383526 14.383287 14.390892 14.381998 14.391005 14.381743 1030: 14.384274 14.381269 14.378385 14.386201 14.400000 14.382556 14.387124 1037: 14.400000 14.384367 14.387065 14.387284 14.379386 14.384733 14.383957 1044: 14.385662 14.388355 14.387666 14.387284 14.379803 14.384597 14.381439 1051: 14.385888 14.381269 source getTriangles = 0, nGtris = 1986, nGsegs = 5958, Ds = 0 0 destin getTriangles = 0, nGtris = 794, nGsegs = 2382, Ds = 0 0 In caps_outputObjects: 2 Analyses found 1 Bounds found testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m10.283s user 0m10.294s sys 0m0.239s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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 0m1.290s user 0m1.149s sys 0m0.117s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected) ============================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/7.7/CAPS/unit/DARWIN_ARM64') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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_UndefinedCaps/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] Obtaining reference build from same job (7.7,CAPS/unit,DARWIN_ARM64,viggen) [Static Analysis] No valid reference build found that meets the criteria (NO_JOB_FAILURE - SUCCESSFUL_QUALITY_GATE) [Static Analysis] All reported issues will be considered outstanding [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #191'. [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