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Skipping 1,157 KB.. Full LogEGADS : 5 Yes 1 -8 11 10 -9 EGADS : 6 Yes 1 12 8 -13 -4 EGADS : 7 Yes 1 -14 6 15 -10 EGADS : 8 Yes 1 7 14 -11 -12 EGADS : 9 Yes 1 -5 13 9 -15 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 1 1 1 2 EGADS : 2 0 Yes 2 2 1 2 3 EGADS : 3 0 Yes 1 2 1 2 2 EGADS : 4 1 Yes 4 3 NA 4 6 EGADS : 5 1 Yes 3 5 NA 4 9 EGADS : 6 1 Yes 6 5 NA 4 7 EGADS : 7 1 Yes 4 6 NA 4 8 EGADS : 8 1 Yes 8 7 NA 5 6 EGADS : 9 1 Yes 7 9 NA 5 9 EGADS : 10 1 Yes 10 9 NA 5 7 EGADS : 11 1 Yes 8 10 NA 5 8 EGADS : 12 1 Yes 4 8 NA 6 8 EGADS : 13 1 Yes 3 7 NA 6 9 EGADS : 14 1 Yes 6 10 NA 7 8 EGADS : 15 1 Yes 5 9 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 2 0 0.5 EGADS : 2 Yes 3 0 0.5 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 100 167 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 105 177 0 AFLR4 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1737 3466 512 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Trias = 1737 3466 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 391 698 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1738 3468 512 OVERALL : CPU Time = 0.101 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 = 1219 Number of elements = 2434 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1738 Total number of elements = 3468 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 .Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 2 Name = Farfield, index = 1 Name = Wing1, index = 2 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 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 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= 17046 33362 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= 17145 33560 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, Trias = 28462 56916 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 15590 30449 0 AFLR4 : Nodes, Trias,Quads= 9447 18163 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15870 31009 0 AFLR4 : Nodes, Trias,Quads= 9438 18145 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= 37390 74772 3650 OVERALL : CPU Time = 4.986 seconds Body 1 (of 1) Number of nodes = 37390 Number of elements = 74772 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 74772 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 37390 Total number of elements = 74772 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 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 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, Trias = 12856 25704 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 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 = 2.181 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 1.23 EGADS : OpenCASCADE Version 7.4.1 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 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 202 370 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 201 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1590 3172 432 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Trias = 1590 3172 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 203 374 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 200 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1592 3176 428 OVERALL : CPU Time = 0.124 seconds Body 1 (of 2) Number of nodes = 373 Number of elements = 742 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 742 Number of quadrilateral elements = 0 Body 2 (of 2) Number of nodes = 1219 Number of elements = 2434 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1592 Total number of elements = 3176 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.23 EGADS : OpenCASCADE Version 7.4.1 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 AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.5 AFLR4 : Min Ref Bounding Box Length = 0.5 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 919 1710 0 AFLR4 : Nodes, Trias,Quads= 675 1222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1830 3656 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Trias = 1830 3656 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 930 1730 0 AFLR4 : Nodes, Trias,Quads= 728 1326 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1882 3760 496 OVERALL : CPU Time = 0.138 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 = 1219 Number of elements = 2434 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2434 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 1882 Total number of elements = 3760 .No analysis directory provided - defaulting to altName Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = Rib_Root, index = 1 Name = Skin, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1 Number of elements = 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 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 = 9607 Number of elements = 19210 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19210 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6142 Number of elements = 12280 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 12280 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 104 Number of elements = 204 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 204 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 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 = 9631 Number of elements = 19254 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19254 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9631 Total number of elements = 19254 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:56407) 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) 16F3FB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 16F3FB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1F939BA80 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1F939BA80 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 = 869 Number of elements = 1734 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1734 Number of quadrilateral elements = 0 Body 3 (of 8) Number of nodes = 1323 Number of elements = 2642 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2642 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 = 824 Number of elements = 1644 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1644 Number of quadrilateral elements = 0 Body 6 (of 8) Number of nodes = 1958 Number of elements = 3916 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3916 Number of quadrilateral elements = 0 Body 7 (of 8) Number of nodes = 945 Number of elements = 1886 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1886 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 = 83235 Total number of elements = 166446 . 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) 1F939BA80 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1F939BA80 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 16F3FB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 16F3FB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1! Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 1958 Number of elements = 3916 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3916 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 = 75688 Total number of elements = 151372 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_3 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = bullet, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 945 Number of elements = 1886 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1886 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 = 74675 Total number of elements = 149342 . 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 = 1323 Number of elements = 2642 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2642 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 = 75053 Total number of elements = 150098 . 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 = 869 Number of elements = 1734 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1734 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 = 74599 Total number of elements = 149190 .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 = 9631 Number of elements = 19254 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19254 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9631 Total number of elements = 19254 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 = 7174 Number of elements = 14340 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 14340 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7174 Total number of elements = 14340 . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_6 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) Body 1 (of 2) Number of nodes = 824 Number of elements = 1644 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1644 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 = 74554 Total number of elements = 149100 . Analysis object with the name, egadsTessAIM, has already been initilized An altName of egadsTessAIM_7 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = torus, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 2) Getting surface mesh for body 2 (of 2) 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 = 7819 Number of elements = 15634 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15634 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5894 Number of elements = 11784 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11784 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 516 Number of elements = 1028 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1028 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14229 Total number of elements = 28446 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 - 14229, elements - 28446 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.735343 Creating surface mesh ... Surface mesh seconds: 0.167327 Recovering boundaries... Boundary recovery seconds: 0.26128 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.140803 Recovering Delaunayness... Delaunay recovery seconds: 0.156698 Refining mesh... 18967 insertions, added 13672 points, 705072 tetrahedra in queue. 6316 insertions, added 2535 points, 591326 tetrahedra in queue. 8419 insertions, added 1784 points, 85235 tetrahedra in queue. Refinement seconds: 10.1372 Smoothing vertices... Mesh smoothing seconds: 8.73982 Improving mesh... Mesh improvement seconds: 0.600668 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.039614 Total running seconds: 20.9833 Statistics: Input points: 14229 Input facets: 28446 Input segments: 42669 Input holes: 2 Input regions: 0 Mesh points: 32940 Mesh tetrahedra: 158672 Mesh faces: 331567 Mesh faces on exterior boundary: 28446 Mesh faces on input facets: 28446 Mesh edges on input segments: 42669 Steiner points inside domain: 18711 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/7.4/CAPS/unit/DARWINM1/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/7.4/CAPS/unit/DARWINM1/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/7.4/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 378, in _readstream self._update_tokens() File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 798, 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/7.4/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/__init__.py", line 31, in read return parser.read(nml_path) File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 281, in read return self._readstream(nml_file, nml_patch) File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/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/7.4/CAPS/unit/DARWINM1/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/7.4/CAPS/unit/DARWINM1/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 Creating FEA BEM Getting quads for BEM! 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 Creating FEA BEM Face 3 quading disabled with attribute .qParams Face 6 quading disabled with attribute .qParams Getting quads for BEM! capsIgnore attribute found for face - 1!! Removing unused nodes... Removed 324 (out of 4009) unused nodes! Mesh for body = 0 Number of nodal coordinates = 3685 Number of elements = 6209 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5126 Elemental Quad4 = 1083 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 Creating FEA BEM Getting quads for BEM! 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 Creating FEA BEM Getting quads for BEM! Mesh for body = 0 Number of nodal coordinates = 400 Number of elements = 361 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 361 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7819 Number of elements = 15634 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15634 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5894 Number of elements = 11784 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11784 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 516 Number of elements = 1028 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1028 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14229 Total number of elements = 28446 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 - 14229, elements - 28446 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.758695 Creating surface mesh ... Surface mesh seconds: 0.166964 Recovering boundaries... Boundary recovery seconds: 0.245745 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.14879 Recovering Delaunayness... Delaunay recovery seconds: 0.151461 Refining mesh... 18967 insertions, added 13672 points, 705072 tetrahedra in queue. 6316 insertions, added 2535 points, 591326 tetrahedra in queue. 8419 insertions, added 1784 points, 85235 tetrahedra in queue. Refinement seconds: 10.2346 Smoothing vertices... Mesh smoothing seconds: 8.93158 Improving mesh... Mesh improvement seconds: 0.638985 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.038388 Total running seconds: 21.3168 Statistics: Input points: 14229 Input facets: 28446 Input segments: 42669 Input holes: 2 Input regions: 0 Mesh points: 32940 Mesh tetrahedra: 158672 Mesh faces: 331567 Mesh faces on exterior boundary: 28446 Mesh faces on input facets: 28446 Mesh edges on input segments: 42669 Steiner points inside domain: 18711 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 "BlackBird (7.4.0) " 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 "BlackBird (7.4.0) " . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... . Running xFoil...... Running xFoil...... . ---------------------------------------------------------------------- Ran 67 tests in 532.561s 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: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! 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 0m0.173s user 0m0.094s sys 0m0.013s ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aimTransferUtilTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/miscUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/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 0m0.171s user 0m0.080s sys 0m0.010s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/miscUtilsTest passed (as expected) ============================================= + expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest + /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest vlmUtils Tests passed! real 0m0.175s user 0m0.084s sys 0m0.011s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest passed (as expected) ============================================= + rm -rf aimTest + expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm Root Path = /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/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/7.4/CAPS/unit/DARWINM1/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 = 2108! testingAIM/aimDiscr: npts = 1113! testingAIM/aimDiscr: tname = Interface, instance = 0! testingAIM/aimDiscr: Tessellation set! testingAIM/aimDiscr: Body 1/Face 6 matches Interface! testingAIM/aimDiscr: ntris = 800! testingAIM/aimDiscr: npts = 447! testingAIM/aimTransfer name = scalar instance = 0 npts = 447/1! 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:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 2 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 2 value = 0.000000 (null) Param has type VALUE, subtype PARAMETER with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 3 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 3 value = 99 (null) num has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 6 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 6 value = 8.000000 (null) x has type VALUE, subtype GEOMETRYIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 7 hist: (null) -> Initial Phase aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 1 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 7 linked to ParamName pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 16 value = 34.641525 (null) cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 16 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 16 value = 7.296560 (null) testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 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:59444 jenkins 2023/02/11 14:02:34 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 8 value = 5.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:34 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 8 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 8 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 8 value (0x0) = NULL with len = 0 writer testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:03:02 18 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 18 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 18 value (0x0) = NULL with len = 0 ego meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 9 testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:02 18 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 18 value = 42 (null) testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 28 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 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:59444 jenkins 2023/02/11 14:02:34 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 10 value = 6.000000 cm table has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 12 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:02:36 18 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 13 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:36 23 linked to tessOut meshFile has type VALUE, subtype ANALYSISIN with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 10 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 10 value (0x0) = NULL with len = 0 writer testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 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:59444 jenkins 2023/02/11 14:03:02 28 tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 11 testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0! tessPtr = 600001440200 value = 600001440200 ego lazy: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:02 28 meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 11 testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0! value (0x0) = NULL with len = 0 writer lazy: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:02 28 Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 28 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 28 value = 42 (null) Interface has type BOUND, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 14 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 2 Connecteds, 0 UnConnecteds testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:38 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:38 23 5 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 1113 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 1113 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 26 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 15 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:03:01 26 1113 points, rank=1, units=(null) testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 6 DataSets xyz has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 447 points, rank=3, units=cm xyzd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 0 points, rank=3, units=(null) param has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 23 447 points, rank=2, units=(null) paramd has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 0 points, rank=2, units=(null) scalar has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 25 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Child Execute aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:40 25 447 points, rank=1, units=(null) vector has type DATASET, subtype NONE with 0 attributes last: aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 hist: (null) -> Starting aimTest VIGGEN.MIT.EDU:59444 jenkins 2023/02/11 14:02:34 0 testingAIM/aimTransfer name = vector instance = 0 npts = 447/3! 447 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 14.380647 14.400000 14.381201 14.400000 15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 22: 14.400000 14.400000 14.390441 14.400000 14.383859 14.400000 14.400000 29: 14.400000 14.400000 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: 14.385061 14.400000 14.383844 14.400000 14.400000 14.400000 14.400000 50: 14.378338 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 57: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.376664 64: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 78: 14.389247 14.400000 14.400000 14.400000 14.400000 14.382317 14.400000 85: 14.400000 14.400000 14.400000 14.390011 14.400000 14.400000 14.400000 92: 14.400000 14.400000 14.400000 14.400000 14.389865 14.400000 14.389101 99: 14.400000 14.388170 14.400000 14.400000 14.400000 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 14.400000 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 14.400000 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 14.400000 14.400000 14.400000 14.400000 14.400000 463: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 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 14.400000 484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 491: 14.400000 14.400000 14.400000 14.400000 14.365872 14.400000 14.400000 498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 505: 14.400000 14.400000 14.400000 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 14.362939 14.400000 14.362723 14.400000 14.400000 14.400000 526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 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: 14.368368 14.400000 14.400000 14.400000 14.400000 14.369831 14.400000 554: 14.400000 14.400000 14.400000 14.368625 14.400000 14.362939 14.400000 561: 14.400000 14.366034 14.400000 14.400000 14.400000 14.400000 14.400000 568: 14.356725 14.400000 14.369831 14.369175 14.400000 14.400000 14.400000 575: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 582: 14.400000 14.363748 14.368368 14.400000 14.400000 14.400000 14.400000 589: 14.369831 14.400000 14.359400 14.400000 14.362294 14.400000 14.400000 596: 14.373876 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 603: 14.369217 14.369217 14.400000 14.365681 14.400000 14.369054 14.400000 610: 14.400000 14.400000 14.400000 14.371385 14.368746 14.372230 14.400000 617: 14.375507 14.400000 14.364430 14.374160 14.400000 14.400000 14.400000 624: 14.368708 14.369354 14.400000 14.400000 14.400000 14.400000 14.400000 631: 14.400000 14.400000 14.370154 14.368219 14.400000 14.372237 14.400000 638: 14.400000 14.374425 14.372363 14.400000 14.400000 14.400000 14.400000 645: 14.375986 14.365557 14.368708 14.366781 14.400000 14.369175 14.369354 652: 14.400000 14.373289 14.400000 14.375685 14.374425 14.400000 14.377582 659: 14.400000 14.400000 14.400000 14.366036 14.400000 14.400000 14.400000 666: 14.400000 14.375124 14.400000 14.400000 14.368903 14.368554 14.400000 673: 14.400000 14.371385 14.371385 14.400000 14.400000 14.379372 14.369129 680: 14.374049 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 687: 14.376399 14.400000 14.377760 14.378863 14.374473 14.367809 14.400000 694: 14.400000 14.368784 14.400000 14.371385 14.365916 14.400000 14.373164 701: 14.400000 14.400000 14.372470 14.400000 14.400000 14.400000 14.400000 708: 14.375986 14.379953 14.400000 14.374316 14.377675 14.400000 14.376295 715: 14.400000 14.400000 14.400000 14.368903 14.368784 14.366475 14.400000 722: 14.400000 14.369555 14.400000 14.378687 14.378687 14.378950 14.400000 729: 14.375449 14.376399 14.371320 14.400000 14.400000 14.371351 14.400000 736: 14.400000 14.375126 14.400000 14.400000 14.400000 14.375504 14.368903 743: 14.368513 14.400000 14.400000 14.400000 14.400000 14.379509 14.375124 750: 14.376289 14.374679 14.400000 14.400000 14.400000 14.400000 14.378601 757: 14.400000 14.377087 14.400000 14.375718 14.373640 14.400000 14.400000 764: 14.372001 14.400000 14.400000 14.368903 14.368513 14.400000 14.374568 771: 14.400000 14.375271 14.400000 14.400000 14.400000 14.400000 14.380017 778: 14.400000 14.400000 14.379331 14.400000 14.400000 14.379693 14.400000 785: 14.372552 14.383094 14.375768 14.400000 14.372608 14.378845 14.400000 792: 14.373363 14.368903 14.400000 14.375189 14.378667 14.375797 14.377675 799: 14.400000 14.400000 14.379863 14.373732 14.400000 14.400000 14.400000 806: 14.400000 14.400000 14.375857 14.400000 14.400000 14.400000 14.400000 813: 14.400000 14.400000 14.400000 14.400000 14.376290 14.379509 14.400000 820: 14.400000 14.400000 14.374594 14.400000 14.376305 14.400000 14.373349 827: 14.400000 14.379553 14.379553 14.373363 14.400000 14.377860 14.382471 834: 14.379565 14.400000 14.376493 14.400000 14.400000 14.400000 14.400000 841: 14.378207 14.375251 14.376604 14.400000 14.378626 14.400000 14.400000 848: 14.400000 14.376156 14.377590 14.379497 14.400000 14.375463 14.378358 855: 14.400000 14.380743 14.375541 14.400000 14.373960 14.400000 14.380592 862: 14.379304 14.374686 14.383536 14.400000 14.400000 14.374081 14.400000 869: 14.400000 14.380716 14.379807 14.383716 14.400000 14.383965 14.377272 876: 14.400000 14.379553 14.400000 14.377569 14.400000 14.376445 14.382213 883: 14.400000 14.400000 14.400000 14.400000 14.371271 14.379704 14.400000 890: 14.400000 14.379157 14.400000 14.379112 14.381121 14.380580 14.400000 897: 14.382553 14.400000 14.383382 14.400000 14.381159 14.400000 14.400000 904: 14.385313 14.382398 14.378148 14.381487 14.400000 14.378926 14.380605 911: 14.400000 14.400000 14.382989 14.384339 14.383216 14.380943 14.382553 918: 14.400000 14.375911 14.400000 14.384096 14.379502 14.376270 14.382299 925: 14.400000 14.380605 14.380605 14.383670 14.382868 14.400000 14.380592 932: 14.400000 14.379140 14.400000 14.400000 14.400000 14.400000 14.379453 939: 14.383433 14.382322 14.382931 14.376461 14.385109 14.386913 14.377699 946: 14.384542 14.400000 14.378601 14.387578 14.400000 14.400000 14.400000 953: 14.385467 14.379641 14.381746 14.383298 14.379930 14.400000 14.381446 960: 14.378196 14.400000 14.400000 14.381473 14.400000 14.383687 14.400000 967: 14.400000 14.384788 14.382697 14.379960 14.382187 14.383771 14.400000 974: 14.376286 14.374476 14.383666 14.382626 14.379930 14.384694 14.384795 981: 14.384528 14.385187 14.382443 14.381568 14.384519 14.385991 14.400000 988: 14.381423 14.400000 14.376098 14.383598 14.400000 14.375887 14.382344 995: 14.400000 14.374828 14.400000 14.386850 14.382671 14.380741 14.377878 1002: 14.388595 14.383868 14.385187 14.400000 14.400000 14.386295 14.384522 1009: 14.388515 14.385094 14.381609 14.387263 14.385337 14.386730 14.386730 1016: 14.387884 14.400000 14.376353 14.377969 14.376461 14.384854 14.378940 1023: 14.400000 14.386177 14.385200 14.385210 14.400000 14.400000 14.388399 1030: 14.384905 14.400000 14.400000 14.385855 14.386303 14.386373 14.389777 1037: 14.383001 14.384393 14.387981 14.400000 14.386362 14.400000 14.400000 1044: 14.400000 14.380951 14.382823 14.381293 14.400000 14.400000 14.375959 1051: 14.380629 14.382255 14.388550 14.385775 14.389044 14.386740 14.385318 1058: 14.400000 14.380768 14.387136 14.385083 14.378339 14.379911 14.379022 1065: 14.400000 14.383818 14.400000 14.373220 14.400000 14.387729 14.382944 1072: 14.387356 14.400000 14.390025 14.387727 14.388858 14.400000 14.381247 1079: 14.386362 14.378339 14.400000 14.400000 14.375685 14.381865 14.383342 1086: 14.386098 14.381327 14.386555 14.381954 14.385445 14.383356 14.384112 1093: 14.379911 14.400000 14.383874 14.400000 14.381637 14.391021 14.400000 1100: 14.400000 14.400000 14.400000 14.400000 14.384655 14.400000 14.378251 1107: 14.400000 14.381756 14.383106 14.386337 14.384313 14.383799 14.384686 source getTriangles = 0, nGtris = 2108, nGsegs = 6324, Ds = 0 0 destin getTriangles = 0, nGtris = 800, nGsegs = 2400, Ds = 0 0 testingAIM/aimCleanup instance = 0! testingAIM/aimCleanup instance = 1! real 0m27.919s user 0m23.800s sys 0m0.208s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm passed (as expected) ============================================= + rm -rf source.vs destin.vs + expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/autoExec testingAIM.csm' + /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/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/7.4/CAPS/unit/DARWINM1/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/7.4/CAPS/unit/DARWINM1/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 0m1.585s user 0m1.242s sys 0m0.093s + set +x ============================================= CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1/ESP/DARWINM1/test/autoExec testingAIM.csm passed (as expected) ============================================= [GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1') [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/7.4/CAPS/unit/DARWINM1') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/unit/DARWINM1') [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/7.4/CAPS/unit/DARWINM1') [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] Reference build recorder is not configured [Static Analysis] Obtaining reference build from same job (7.4,CAPS/unit,DARWINM1,viggen) [Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/unit,ESP_ARCH=DARWINM1,buildnode=viggen #175' to compute new, fixed, and outstanding issues [Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0 [Static Analysis] Evaluating quality gates [Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1 [Static Analysis] -> All quality gates have been passed [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/unit,ESP_ARCH=DARWINM1,buildnode=viggen #176'. [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