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Full LogAFLR4 : Nodes, Trias,Quads= 132 223 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 99 158 0 AFLR4 : Nodes, Trias,Quads= 127 214 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 116 197 0 AFLR4 : Nodes, Trias,Quads= 107 179 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 977 1820 0 AFLR4 : Nodes, Trias,Quads= 797 1460 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 200 368 0 AFLR4 : Generate optimal mesh on surface definition 15 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 197 362 0 AFLR4 : Generate optimal mesh on surface definition 16 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 17 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 18 AFLR2 : Nodes, Trias,Quads= 320 562 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 19 AFLR2 : Nodes, Trias,Quads= 319 560 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 20 AFLR2 : Nodes, Trias,Quads= 319 560 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 21 AFLR2 : Nodes, Trias,Quads= 319 560 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= 3194 6368 870 OVERALL : CPU Time = 0.269 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 6) Number of nodes = 43 Number of elements = 82 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 82 Number of quadrilateral elements = 0 Body 2 (of 6) Number of nodes = 525 Number of elements = 1046 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1046 Number of quadrilateral elements = 0 Body 3 (of 6) Number of nodes = 310 Number of elements = 616 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 616 Number of quadrilateral elements = 0 Body 4 (of 6) Number of nodes = 730 Number of elements = 1460 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1460 Number of quadrilateral elements = 0 Body 5 (of 6) Number of nodes = 367 Number of elements = 730 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 730 Number of quadrilateral elements = 0 Body 6 (of 6) 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 = 3194 Total number of elements = 6368 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_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 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 6 Faces EGADS : Body 0 has 12 Edges EGADS : Body 0 has 6 Loops EGADS : Body 0 has 8 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 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 3 4 5 6 EGADS : 2 Yes 0 0 1 0 1 3 4 5 6 EGADS : 3 Yes 0 0 1 0 1 1 2 5 6 EGADS : 4 Yes 0 0 1 0 1 1 2 5 6 EGADS : 5 Yes 0 0 1 0 1 1 2 3 4 EGADS : 6 Yes 0 0 1 0 1 1 2 3 4 EGADS : 7 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 8 Yes 1 0 1 NA NA 9 10 11 12 EGADS : 9 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 10 Yes 1 0 1 NA NA 7 8 11 12 EGADS : 11 Yes 1 0 1 NA NA 7 8 9 10 EGADS : 12 Yes 1 0 1 NA NA 7 8 9 10 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 -5 8 7 -6 EGADS : 3 9 5 -10 -1 EGADS : 4 -11 3 12 -7 EGADS : 5 4 11 -8 -9 EGADS : 6 -2 10 6 -12 EGADS : 7 13 14 -15 -16 EGADS : 8 -17 20 19 -18 EGADS : 9 21 17 -22 -13 EGADS : 10 -23 15 24 -19 EGADS : 11 16 23 -20 -21 EGADS : 12 -14 22 18 -24 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 : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 -5 8 7 -6 EGADS : 3 Yes 1 9 5 -10 -1 EGADS : 4 Yes 1 -11 3 12 -7 EGADS : 5 Yes 1 4 11 -8 -9 EGADS : 6 Yes 1 -2 10 6 -12 EGADS : 7 Yes 1 13 14 -15 -16 EGADS : 8 Yes 1 -17 20 19 -18 EGADS : 9 Yes 1 21 17 -22 -13 EGADS : 10 Yes 1 -23 15 24 -19 EGADS : 11 Yes 1 16 23 -20 -21 EGADS : 12 Yes 1 -14 22 18 -24 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 1 1 3 EGADS : 2 0 Yes 1 3 1 1 6 EGADS : 3 0 Yes 4 3 1 1 4 EGADS : 4 0 Yes 2 4 1 1 5 EGADS : 5 0 Yes 6 5 1 2 3 EGADS : 6 0 Yes 5 7 1 2 6 EGADS : 7 0 Yes 8 7 1 2 4 EGADS : 8 0 Yes 6 8 1 2 5 EGADS : 9 0 Yes 2 6 1 3 5 EGADS : 10 0 Yes 1 5 1 3 6 EGADS : 11 0 Yes 4 8 1 4 5 EGADS : 12 0 Yes 3 7 1 4 6 EGADS : 13 1 Yes 10 9 NA 7 9 EGADS : 14 1 Yes 9 11 NA 7 12 EGADS : 15 1 Yes 12 11 NA 7 10 EGADS : 16 1 Yes 10 12 NA 7 11 EGADS : 17 1 Yes 14 13 NA 8 9 EGADS : 18 1 Yes 13 15 NA 8 12 EGADS : 19 1 Yes 16 15 NA 8 10 EGADS : 20 1 Yes 14 16 NA 8 11 EGADS : 21 1 Yes 10 14 NA 9 11 EGADS : 22 1 Yes 9 13 NA 9 12 EGADS : 23 1 Yes 12 16 NA 10 11 EGADS : 24 1 Yes 11 15 NA 10 12 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 0.5 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 0.5 0.5 EGADS : 4 Yes 0 0.5 0 EGADS : 5 Yes 1 0 0.5 EGADS : 6 Yes 1 0 0 EGADS : 7 Yes 1 0.5 0.5 EGADS : 8 Yes 1 0.5 0 EGADS : 9 Yes 0 0 2 EGADS : 10 Yes 0 0 0 EGADS : 11 Yes 0 2 2 EGADS : 12 Yes 0 2 0 EGADS : 13 Yes 14 0 2 EGADS : 14 Yes 14 0 0 EGADS : 15 Yes 14 2 2 EGADS : 16 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 STD w/BL AFLR4 : 5 CAD geometry 0 STD w/BL AFLR4 : 6 CAD geometry 0 STD w/BL AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : 10 CAD geometry 0 FARFIELD AFLR4 : 11 CAD geometry 0 FARFIELD AFLR4 : 12 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 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 12 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= 1239 2470 416 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1239 2470 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 12 14 0 AFLR4 : Nodes, Trias,Quads= 8 6 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 12 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= 1239 2470 416 OVERALL : CPU Time = 0.061 seconds Body 1 (of 2) Number of nodes = 20 Number of elements = 36 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 36 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 = 1239 Total number of elements = 2470 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_2 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 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 5 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 3 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 3 -2 -3 EGADS : 2 2 5 -4 -5 EGADS : 3 4 EGADS : 4 6 7 -8 -9 EGADS : 5 -10 13 12 -11 EGADS : 6 14 10 -15 -6 EGADS : 7 -16 8 17 -12 EGADS : 8 9 16 -13 -14 EGADS : 9 -7 15 11 -17 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 3 -2 -3 EGADS : 2 Yes 1 2 5 -4 -5 EGADS : 3 Yes 1 4 EGADS : 4 Yes 1 6 7 -8 -9 EGADS : 5 Yes 1 -10 13 12 -11 EGADS : 6 Yes 1 14 10 -15 -6 EGADS : 7 Yes 1 -16 8 17 -12 EGADS : 8 Yes 1 9 16 -13 -14 EGADS : 9 Yes 1 -7 15 11 -17 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 2 1 1 2 EGADS : 3 0 Yes 1 2 1 1 1 EGADS : 4 0 Yes 3 3 1 2 3 EGADS : 5 0 Yes 2 3 1 2 2 EGADS : 6 1 Yes 5 4 NA 4 6 EGADS : 7 1 Yes 4 6 NA 4 9 EGADS : 8 1 Yes 7 6 NA 4 7 EGADS : 9 1 Yes 5 7 NA 4 8 EGADS : 10 1 Yes 9 8 NA 5 6 EGADS : 11 1 Yes 8 10 NA 5 9 EGADS : 12 1 Yes 11 10 NA 5 7 EGADS : 13 1 Yes 9 11 NA 5 8 EGADS : 14 1 Yes 5 9 NA 6 8 EGADS : 15 1 Yes 4 8 NA 6 9 EGADS : 16 1 Yes 7 11 NA 7 8 EGADS : 17 1 Yes 6 10 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 12 0 0 EGADS : 2 Yes 12.18062 0 0 EGADS : 3 Yes 13.3304132 0 0 EGADS : 4 Yes 0 0 2 EGADS : 5 Yes 0 0 0 EGADS : 6 Yes 0 2 2 EGADS : 7 Yes 0 2 0 EGADS : 8 Yes 14 0 2 EGADS : 9 Yes 14 0 0 EGADS : 10 Yes 14 2 2 EGADS : 11 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.33041 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= 37 48 0 AFLR4 : Nodes, Trias,Quads= 56 86 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 304 535 0 AFLR4 : Nodes, Trias,Quads= 366 659 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 102 171 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= 1679 3350 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1679 3350 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 40 53 0 AFLR4 : Nodes, Trias,Quads= 55 83 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 320 564 0 AFLR4 : Nodes, Trias,Quads= 381 686 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 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= 1688 3368 498 OVERALL : CPU Time = 0.083 seconds Body 1 (of 2) Number of nodes = 469 Number of elements = 934 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 934 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 = 1688 Total number of elements = 3368 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_3 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 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 6 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 3 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 3 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 -2 3 4 EGADS : 2 5 2 -6 -4 EGADS : 3 1 6 EGADS : 4 7 8 -9 -10 EGADS : 5 -11 14 13 -12 EGADS : 6 15 11 -16 -7 EGADS : 7 -17 9 18 -13 EGADS : 8 10 17 -14 -15 EGADS : 9 -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 : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 -2 3 4 EGADS : 2 Yes 1 5 2 -6 -4 EGADS : 3 Yes 1 1 6 EGADS : 4 Yes 1 7 8 -9 -10 EGADS : 5 Yes 1 -11 14 13 -12 EGADS : 6 Yes 1 15 11 -16 -7 EGADS : 7 Yes 1 -17 9 18 -13 EGADS : 8 Yes 1 10 17 -14 -15 EGADS : 9 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 Yes 2 1 1 1 3 EGADS : 2 0 Yes 3 2 1 1 2 EGADS : 3 0 DEGEN 3 3 - 1 EGADS : 4 0 Yes 3 1 1 1 2 EGADS : 5 0 DEGEN 3 3 - 2 EGADS : 6 0 Yes 1 2 1 2 3 EGADS : 7 1 Yes 5 4 NA 4 6 EGADS : 8 1 Yes 4 6 NA 4 9 EGADS : 9 1 Yes 7 6 NA 4 7 EGADS : 10 1 Yes 5 7 NA 4 8 EGADS : 11 1 Yes 9 8 NA 5 6 EGADS : 12 1 Yes 8 10 NA 5 9 EGADS : 13 1 Yes 11 10 NA 5 7 EGADS : 14 1 Yes 9 11 NA 5 8 EGADS : 15 1 Yes 5 9 NA 6 8 EGADS : 16 1 Yes 4 8 NA 6 9 EGADS : 17 1 Yes 7 11 NA 7 8 EGADS : 18 1 Yes 6 10 NA 7 9 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 5 0 0 EGADS : 2 Yes 5 0 0.5 EGADS : 3 Yes 4 0 0 EGADS : 4 Yes 0 0 2 EGADS : 5 Yes 0 0 0 EGADS : 6 Yes 0 2 2 EGADS : 7 Yes 0 2 0 EGADS : 8 Yes 14 0 2 EGADS : 9 Yes 14 0 0 EGADS : 10 Yes 14 2 2 EGADS : 11 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 104 168 0 AFLR4 : Nodes, Trias,Quads= 124 208 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 104 168 0 AFLR4 : Nodes, Trias,Quads= 123 206 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 112 190 0 AFLR4 : Nodes, Trias,Quads= 95 156 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= 1506 3004 476 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1506 3004 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 101 162 0 AFLR4 : Nodes, Trias,Quads= 129 218 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 102 164 0 AFLR4 : Nodes, Trias,Quads= 127 214 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 111 188 0 AFLR4 : Nodes, Trias,Quads= 103 172 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= 1523 3038 476 OVERALL : CPU Time = 0.064 seconds Body 1 (of 2) Number of nodes = 304 Number of elements = 604 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 604 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 = 1523 Total number of elements = 3038 . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_4 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = cylinder, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 3 Faces EGADS : Body 0 has 3 Edges EGADS : Body 0 has 3 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 EGADS : 2 Yes 0 0 1 0 1 1 3 EGADS : 3 Yes 0 0 1 0 1 2 EGADS : 4 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 5 Yes 1 0 1 NA NA 6 7 8 9 EGADS : 6 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 7 Yes 1 0 1 NA NA 4 5 8 9 EGADS : 8 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 9 Yes 1 0 1 NA NA 4 5 6 7 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 EGADS : 2 1 3 -2 -3 EGADS : 3 2 EGADS : 4 4 5 -6 -7 EGADS : 5 -8 11 10 -9 EGADS : 6 12 8 -13 -4 EGADS : 7 -14 6 15 -10 EGADS : 8 7 14 -11 -12 EGADS : 9 -5 13 9 -15 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 EGADS : 2 Yes 1 1 3 -2 -3 EGADS : 3 Yes 1 2 EGADS : 4 Yes 1 4 5 -6 -7 EGADS : 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 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 STD w/BL AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : 9 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Nodes, Trias,Quads= 100 167 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 105 177 0 AFLR4 : Nodes, Trias,Quads= 103 173 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1737 3466 512 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1737 3466 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 104 175 0 AFLR4 : Nodes, Trias,Quads= 99 165 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 388 692 0 AFLR4 : Nodes, Trias,Quads= 391 698 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Nodes, Trias,Quads= 102 171 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1738 3468 512 OVERALL : CPU Time = 0.072 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 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 5 6 -7 -1 EGADS : 3 Yes 1 -2 7 9 -8 EGADS : 4 Yes 1 -10 3 8 -11 EGADS : 5 Yes 1 4 10 -12 -5 EGADS : 6 Yes 1 -6 12 11 -9 EGADS : 7 Yes 1 -13 14 15 -16 EGADS : 8 Yes 1 -17 18 13 -19 EGADS : 9 Yes 1 20 22 -21 -14 EGADS : 10 Yes 1 -15 23 17 -24 EGADS : 11 Yes 1 16 24 19 EGADS : 12 Yes 1 25 26 -20 -18 EGADS : 13 Yes 1 21 27 -25 -23 EGADS : 14 Yes 1 -22 -26 -27 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 2.82843 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.60986 AFLR4 : Abs Min Surf Spacing = 0.00707107 AFLR4 : Min Surf Spacing = 0.0141421 AFLR4 : Max Surf Spacing = 0.282843 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 17049 33368 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= 17143 33556 0 AFLR4 : Nodes, Trias,Quads= 7368 14006 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 14987 29245 0 AFLR4 : Nodes, Trias,Quads= 6879 13029 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 330 546 0 AFLR4 : Nodes, Trias,Quads= 322 530 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 182 241 0 AFLR4 : Nodes, Trias,Quads= 122 121 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 14793 28857 0 AFLR4 : Nodes, Trias,Quads= 6844 12959 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 328 542 0 AFLR4 : Nodes, Trias,Quads= 324 534 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 28462 56916 3616 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 28462 56916 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 137 232 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 15590 30449 0 AFLR4 : Nodes, Trias,Quads= 9447 18163 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 254 370 0 AFLR4 : Nodes, Trias,Quads= 136 134 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 15870 31009 0 AFLR4 : Nodes, Trias,Quads= 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 = 1.716 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 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 1 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 2 Shells EGADS : Body 0 has 14 Faces EGADS : Body 0 has 27 Edges EGADS : Body 0 has 14 Loops EGADS : Body 0 has 17 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6 EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6 EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 0 0 1 0 1 8 9 10 11 EGADS : 8 Yes 0 0 1 0 1 7 10 11 12 EGADS : 9 Yes 0 0 1 0 1 7 12 13 14 EGADS : 10 Yes 0 0 1 0 1 7 8 11 13 EGADS : 11 Yes 0 0 1 0 1 7 8 10 EGADS : 12 Yes 0 0 1 0 1 8 9 13 14 EGADS : 13 Yes 0 0 1 0 1 9 10 12 14 EGADS : 14 Yes 0 0 1 0 1 9 12 13 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 1 2 -3 -4 EGADS : 2 5 6 -7 -1 EGADS : 3 -2 7 9 -8 EGADS : 4 -10 3 8 -11 EGADS : 5 4 10 -12 -5 EGADS : 6 -6 12 11 -9 EGADS : 7 -13 14 15 -16 EGADS : 8 -17 18 13 -19 EGADS : 9 20 22 -21 -14 EGADS : 10 -15 23 17 -24 EGADS : 11 16 24 19 EGADS : 12 25 26 -20 -18 EGADS : 13 21 27 -25 -23 EGADS : 14 -22 -26 -27 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : 9 9 EGADS : 10 10 EGADS : 11 11 EGADS : 12 12 EGADS : 13 13 EGADS : 14 14 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 1 2 -3 -4 EGADS : 2 Yes 1 5 6 -7 -1 EGADS : 3 Yes 1 -2 7 9 -8 EGADS : 4 Yes 1 -10 3 8 -11 EGADS : 5 Yes 1 4 10 -12 -5 EGADS : 6 Yes 1 -6 12 11 -9 EGADS : 7 Yes 1 -13 14 15 -16 EGADS : 8 Yes 1 -17 18 13 -19 EGADS : 9 Yes 1 20 22 -21 -14 EGADS : 10 Yes 1 -15 23 17 -24 EGADS : 11 Yes 1 16 24 19 EGADS : 12 Yes 1 25 26 -20 -18 EGADS : 13 Yes 1 21 27 -25 -23 EGADS : 14 Yes 1 -22 -26 -27 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 2 1 NA 1 2 EGADS : 2 0 Yes 1 3 NA 1 3 EGADS : 3 0 Yes 4 3 NA 1 4 EGADS : 4 0 Yes 2 4 NA 1 5 EGADS : 5 0 Yes 2 5 NA 2 5 EGADS : 6 0 Yes 5 6 NA 2 6 EGADS : 7 0 Yes 1 6 NA 2 3 EGADS : 8 0 Yes 3 7 NA 3 4 EGADS : 9 0 Yes 6 7 NA 3 6 EGADS : 10 0 Yes 4 8 NA 4 5 EGADS : 11 0 Yes 8 7 NA 4 6 EGADS : 12 0 Yes 5 8 NA 5 6 EGADS : 13 0 Yes 9 10 1 7 8 EGADS : 14 0 Yes 9 11 1 7 9 EGADS : 15 0 Yes 11 12 1 7 10 EGADS : 16 0 Yes 10 12 1 7 11 EGADS : 17 0 Yes 13 14 1 8 10 EGADS : 18 0 Yes 13 9 1 8 12 EGADS : 19 0 Yes 14 10 1 8 11 EGADS : 20 0 Yes 9 15 1 9 12 EGADS : 21 0 Yes 11 16 1 9 13 EGADS : 22 0 Yes 15 16 1 9 14 EGADS : 23 0 Yes 11 13 1 10 13 EGADS : 24 0 Yes 12 14 1 10 11 EGADS : 25 0 Yes 13 17 1 12 13 EGADS : 26 0 Yes 17 15 1 12 14 EGADS : 27 0 Yes 16 17 1 13 14 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 0 0 40 EGADS : 2 Yes 0 0 0 EGADS : 3 Yes 0 40 40 EGADS : 4 Yes 0 40 0 EGADS : 5 Yes 40 0 0 EGADS : 6 Yes 40 0 40 EGADS : 7 Yes 40 40 40 EGADS : 8 Yes 40 40 0 EGADS : 9 Yes 3.77246052 0 0.00459131419 EGADS : 10 Yes 5.90487498 7.07106781 0 EGADS : 11 Yes 0 0 0 EGADS : 12 Yes 4.0824829 7.07106781 0.123425948 EGADS : 13 Yes 3.77001182 0 0 EGADS : 14 Yes 5.90282524 7.07106781 0 EGADS : 15 Yes 5.90487498 0 0 EGADS : 16 Yes 4.0824829 0 0.123425948 EGADS : 17 Yes 5.90282524 0 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 80 AFLR4 : Min Bounding Box Length = 80 AFLR4 : Max Ref Bounding Box Length = 14.1421 AFLR4 : Min Ref Bounding Box Length = 0.890888 AFLR4 : Reference Length = 5.65685 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 7.62074 AFLR4 : Abs Min Surf Spacing = 0.0141421 AFLR4 : Min Surf Spacing = 0.0282843 AFLR4 : Max Surf Spacing = 0.565685 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 FARFIELD AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 STD w/BL AFLR4 : 8 CAD geometry 0 STD w/BL AFLR4 : 9 CAD geometry 0 STD w/BL AFLR4 : 10 CAD geometry 0 STD w/BL AFLR4 : 11 CAD geometry 0 STD w/BL AFLR4 : 12 CAD geometry 0 STD w/BL AFLR4 : 13 CAD geometry 0 STD w/BL AFLR4 : 14 CAD geometry 0 STD w/BL AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Define CAD surface definition 9 AFLR4 : Define CAD surface definition 10 AFLR4 : Define CAD surface definition 11 AFLR4 : Define CAD surface definition 12 AFLR4 : Define CAD surface definition 13 AFLR4 : Define CAD surface definition 14 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 136 230 0 AFLR4 : Nodes, Trias,Quads= 132 222 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 6411 12401 0 AFLR4 : Nodes, Trias,Quads= 3253 6085 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 9 AFLR2 : Nodes, Trias,Quads= 6519 12617 0 AFLR4 : Nodes, Trias,Quads= 3180 5939 0 AFLR4 : Generate optimal mesh on surface definition 10 AFLR2 : Nodes, Trias,Quads= 5814 11207 0 AFLR4 : Nodes, Trias,Quads= 3048 5675 0 AFLR4 : Generate optimal mesh on surface definition 11 AFLR2 : Nodes, Trias,Quads= 257 412 0 AFLR4 : Nodes, Trias,Quads= 256 410 0 AFLR4 : Generate optimal mesh on surface definition 12 AFLR2 : Nodes, Trias,Quads= 192 273 0 AFLR4 : Nodes, Trias,Quads= 110 109 0 AFLR4 : Generate optimal mesh on surface definition 13 AFLR2 : Nodes, Trias,Quads= 5862 11303 0 AFLR4 : Nodes, Trias,Quads= 3028 5635 0 AFLR4 : Generate optimal mesh on surface definition 14 AFLR2 : Nodes, Trias,Quads= 258 414 0 AFLR4 : Nodes, Trias,Quads= 256 410 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 12856 25704 2334 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 12856 25704 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 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 = 0.782 seconds Body 1 (of 1) Number of nodes = 18601 Number of elements = 37194 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 37194 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 18601 Total number of elements = 37194 . EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! . Analysis object with the name, aflr4AIM, has already been initilized An altName of aflr4AIM_5 will be used! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = sphere, index = 1 Name = farfield, index = 2 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 EGADS : --------------------------------------- EGADS : Engineering Geometry Aircraft Design System EGADS : Version 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 2 Faces EGADS : Body 0 has 6 Edges EGADS : Body 0 has 2 Loops EGADS : Body 0 has 2 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 2 EGADS : 2 Yes 0 0 1 0 1 1 EGADS : 3 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 4 Yes 1 0 1 NA NA 5 6 7 8 EGADS : 5 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 6 Yes 1 0 1 NA NA 3 4 7 8 EGADS : 7 Yes 1 0 1 NA NA 3 4 5 6 EGADS : 8 Yes 1 0 1 NA NA 3 4 5 6 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 -2 3 4 EGADS : 2 -5 -4 6 2 EGADS : 3 7 8 -9 -10 EGADS : 4 -11 14 13 -12 EGADS : 5 15 11 -16 -7 EGADS : 6 -17 9 18 -13 EGADS : 7 10 17 -14 -15 EGADS : 8 -8 16 12 -18 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : 8 8 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 -2 3 4 EGADS : 2 Yes 1 -5 -4 6 2 EGADS : 3 Yes 1 7 8 -9 -10 EGADS : 4 Yes 1 -11 14 13 -12 EGADS : 5 Yes 1 15 11 -16 -7 EGADS : 6 Yes 1 -17 9 18 -13 EGADS : 7 Yes 1 10 17 -14 -15 EGADS : 8 Yes 1 -8 16 12 -18 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 DEGEN 1 1 - 1 EGADS : 2 0 Yes 2 1 1 1 2 EGADS : 3 0 DEGEN 2 2 - 1 EGADS : 4 0 Yes 2 1 1 1 2 EGADS : 5 0 DEGEN 1 1 - 2 EGADS : 6 0 DEGEN 2 2 - 2 EGADS : 7 1 Yes 4 3 NA 3 5 EGADS : 8 1 Yes 3 5 NA 3 8 EGADS : 9 1 Yes 6 5 NA 3 6 EGADS : 10 1 Yes 4 6 NA 3 7 EGADS : 11 1 Yes 8 7 NA 4 5 EGADS : 12 1 Yes 7 9 NA 4 8 EGADS : 13 1 Yes 10 9 NA 4 6 EGADS : 14 1 Yes 8 10 NA 4 7 EGADS : 15 1 Yes 4 8 NA 5 7 EGADS : 16 1 Yes 3 7 NA 5 8 EGADS : 17 1 Yes 6 10 NA 6 7 EGADS : 18 1 Yes 5 9 NA 6 8 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 8.5 0 0.5 EGADS : 2 Yes 8.5 0 0 EGADS : 3 Yes 0 0 2 EGADS : 4 Yes 0 0 0 EGADS : 5 Yes 0 2 2 EGADS : 6 Yes 0 2 0 EGADS : 7 Yes 14 0 2 EGADS : 8 Yes 14 0 0 EGADS : 9 Yes 14 2 2 EGADS : 10 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1 AFLR4 : Min Ref Bounding Box Length = 1 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 STD w/BL AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : 8 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Define CAD surface definition 8 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 202 370 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 94 154 0 AFLR4 : Nodes, Trias,Quads= 201 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1590 3172 432 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1590 3172 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 203 374 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 81 130 0 AFLR4 : Nodes, Trias,Quads= 200 368 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 8 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1592 3176 428 OVERALL : CPU Time = 0.137 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 1.25 EGADS : OpenCASCADE Version 7.8.0 EGADS : --------------------------------------- EGADS : EGADS CAD Geometry Setup EGADS : Model has 2 Active Bodies EGADS : Body 0 is a SolidBody EGADS : Body 0 has 1 Shells EGADS : Body 0 has 1 Faces EGADS : Body 0 has 2 Edges EGADS : Body 0 has 1 Loops EGADS : Body 0 has 1 Nodes EGADS : Body 1 is a SolidBody EGADS : Body 1 has 1 Shells EGADS : Body 1 has 6 Faces EGADS : Body 1 has 12 Edges EGADS : Body 1 has 6 Loops EGADS : Body 1 has 8 Nodes EGADS : Check Grid BCs EGADS : Grid BCs are OK EGADS : Face Neighbor-Faces Information EGADS : QC = Face Quad Combination Flag EGADS : IER = Face Isolated Edge Refinement Flag EGADS : ER = Face Edge Refinement Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : SF = Face Scale Factor EGADS : Not applicable for Faces with a FarField Grid BC. EGADS : Face Body QC IER ER Scale Neighbor EGADS : ID Active ID Flag Flag Weight Factor Faces EGADS : 1 Yes 0 0 1 0 1 EGADS : 2 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 3 Yes 1 0 1 NA NA 4 5 6 7 EGADS : 4 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 5 Yes 1 0 1 NA NA 2 3 6 7 EGADS : 6 Yes 1 0 1 NA NA 2 3 4 5 EGADS : 7 Yes 1 0 1 NA NA 2 3 4 5 EGADS : Face Edges Information EGADS : Face Edges EGADS : 1 -1 2 1 -2 EGADS : 2 3 4 -5 -6 EGADS : 3 -7 10 9 -8 EGADS : 4 11 7 -12 -3 EGADS : 5 -13 5 14 -9 EGADS : 6 6 13 -10 -11 EGADS : 7 -4 12 8 -14 EGADS : Face Loops Information EGADS : Face Loops EGADS : 1 1 EGADS : 2 2 EGADS : 3 3 EGADS : 4 4 EGADS : 5 5 EGADS : 6 6 EGADS : 7 7 EGADS : Loop Edges Information EGADS : Loop Active Sense Edges EGADS : 1 Yes 1 -1 2 1 -2 EGADS : 2 Yes 1 3 4 -5 -6 EGADS : 3 Yes 1 -7 10 9 -8 EGADS : 4 Yes 1 11 7 -12 -3 EGADS : 5 Yes 1 -13 5 14 -9 EGADS : 6 Yes 1 6 13 -10 -11 EGADS : 7 Yes 1 -4 12 8 -14 EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information EGADS : ESF = Edge Scale Factor EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField EGADS : Grid BC Neighbor Face. EGADS : Neighbor EGADS : Edge Body Active Node1 Node2 ESF Faces EGADS : 1 0 Yes 1 1 1 1 1 EGADS : 2 0 Yes 1 1 1 1 1 EGADS : 3 1 Yes 3 2 NA 2 4 EGADS : 4 1 Yes 2 4 NA 2 7 EGADS : 5 1 Yes 5 4 NA 2 5 EGADS : 6 1 Yes 3 5 NA 2 6 EGADS : 7 1 Yes 7 6 NA 3 4 EGADS : 8 1 Yes 6 8 NA 3 7 EGADS : 9 1 Yes 9 8 NA 3 5 EGADS : 10 1 Yes 7 9 NA 3 6 EGADS : 11 1 Yes 3 7 NA 4 6 EGADS : 12 1 Yes 2 6 NA 4 7 EGADS : 13 1 Yes 5 9 NA 5 6 EGADS : 14 1 Yes 4 8 NA 5 7 EGADS : Node Information EGADS : Node Active Coordinates EGADS : 1 Yes 7.25 0 0 EGADS : 2 Yes 0 0 2 EGADS : 3 Yes 0 0 0 EGADS : 4 Yes 0 2 2 EGADS : 5 Yes 0 2 0 EGADS : 6 Yes 14 0 2 EGADS : 7 Yes 14 0 0 EGADS : 8 Yes 14 2 2 EGADS : 9 Yes 14 2 0 EGADS : Face and Edge Match Information EGADS : No Face Matches Found AFLR4 : Surface Mesh Spacing Setup AFLR4 : Max Bounding Box Length = 15 AFLR4 : Min Bounding Box Length = 4 AFLR4 : Max Ref Bounding Box Length = 1.5 AFLR4 : Min Ref Bounding Box Length = 0.5 AFLR4 : Reference Length = 1 AFLR4 : BL Thickness = 0 AFLR4 : FarField Spacing = 0.5 AFLR4 : Abs Min Surf Spacing = 0.0025 AFLR4 : Min Surf Spacing = 0.1 AFLR4 : Max Surf Spacing = 0.5 AFLR4 : Global Scale Factor = 1 AFLR4 : Geometry Definition Information AFLR4 : Definition Definition Composite Grid BC AFLR4 : ID Type ID Type AFLR4 : 0 glue-only composite - - AFLR4 : 1 CAD geometry 0 STD w/BL AFLR4 : 2 CAD geometry 0 FARFIELD AFLR4 : 3 CAD geometry 0 FARFIELD AFLR4 : 4 CAD geometry 0 FARFIELD AFLR4 : 5 CAD geometry 0 FARFIELD AFLR4 : 6 CAD geometry 0 FARFIELD AFLR4 : 7 CAD geometry 0 FARFIELD AFLR4 : Define CAD surface definition 1 AFLR4 : Define CAD surface definition 2 AFLR4 : Define CAD surface definition 3 AFLR4 : Define CAD surface definition 4 AFLR4 : Define CAD surface definition 5 AFLR4 : Define CAD surface definition 6 AFLR4 : Define CAD surface definition 7 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 919 1710 0 AFLR4 : Nodes, Trias,Quads= 675 1222 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 312 546 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 311 544 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1830 3656 494 AFLR4 : Curvature BG Surface Grid Generation AFLR4 : Nodes, Faces = 1830 3656 AFLR4 : Surface Grid Generation AFLR4 : Generate optimal mesh on surface definition 1 AFLR2 : Nodes, Trias,Quads= 930 1730 0 AFLR4 : Nodes, Trias,Quads= 728 1326 0 AFLR4 : Generate optimal mesh on surface definition 2 AFLR2 : Nodes, Trias,Quads= 91 148 0 AFLR4 : Nodes, Trias,Quads= 88 142 0 AFLR4 : Generate optimal mesh on surface definition 3 AFLR2 : Nodes, Trias,Quads= 92 150 0 AFLR4 : Nodes, Trias,Quads= 87 140 0 AFLR4 : Generate optimal mesh on surface definition 4 AFLR2 : Nodes, Trias,Quads= 313 548 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 5 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 6 AFLR2 : Nodes, Trias,Quads= 310 542 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 AFLR4 : Generate optimal mesh on surface definition 7 AFLR2 : Nodes, Trias,Quads= 314 550 0 AFLR4 : Nodes, Trias,Quads= 308 538 0 DGEOM : Add surface definitions to composite definition 0 DGEOM : Glue composite surface definition 0 DGEOM : Nodes,Faces,BEdges= 1882 3760 496 OVERALL : CPU Time = 0.110 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 .ssMapping 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 = 9581 Number of elements = 19158 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19158 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 6154 Number of elements = 12304 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 12304 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 120 Number of elements = 236 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 236 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 15855 Total number of elements = 31698 .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 = 9625 Number of elements = 19242 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19242 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9625 Total number of elements = 19242 .ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61202) Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 8 Name = box, index = 1 Name = cylinder, index = 2 Name = cone, index = 3 Name = torus, index = 4 Name = sphere, index = 5 Name = boxhole, index = 6 Name = bullet, index = 7 Name = farfield, index = 8 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 0 Getting surface mesh for body 1 (of 8) Getting surface mesh for body 2 (of 8) Getting surface mesh for body 3 (of 8) Getting surface mesh for body 4 (of 8) Getting surface mesh for body 5 (of 8) Getting surface mesh for body 6 (of 8) 1804 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1804 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1AF0 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1AF0 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 = 876 Number of elements = 1748 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1748 Number of quadrilateral elements = 0 Body 3 (of 8) Number of nodes = 1319 Number of elements = 2634 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2634 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 = 1961 Number of elements = 3922 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3922 Number of quadrilateral elements = 0 Body 7 (of 8) Number of nodes = 933 Number of elements = 1862 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1862 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 = 83229 Total number of elements = 166434 . 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) 1804 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1! 1804 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1! 1854 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1! 1854 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 = 1961 Number of elements = 3922 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 3922 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 = 75691 Total number of elements = 151378 . 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 = 933 Number of elements = 1862 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1862 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 = 74663 Total number of elements = 149318 . 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 = 1319 Number of elements = 2634 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 2634 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 = 75049 Total number of elements = 150090 . 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 = 876 Number of elements = 1748 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1748 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 = 74606 Total number of elements = 149204 .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 = 9625 Number of elements = 19242 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 19242 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 9625 Total number of elements = 19242 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 = 7130 Number of elements = 14252 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 14252 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 7130 Total number of elements = 14252 . 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 = 7750 Number of elements = 15496 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15496 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5870 Number of elements = 11736 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11736 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 522 Number of elements = 1040 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1040 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14142 Total number of elements = 28272 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 - 14142, elements - 28272 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.308 Creating surface mesh ... Surface mesh seconds: 0.076 Recovering boundaries... Boundary recovery seconds: 0.231 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.134 Recovering Delaunayness... Delaunay recovery seconds: 0.108 Refining mesh... 18851 insertions, added 13350 points, 706982 tetrahedra in queue. 6277 insertions, added 2016 points, 692557 tetrahedra in queue. 8367 insertions, added 2428 points, 526276 tetrahedra in queue. Refinement seconds: 4.332 Smoothing vertices... Mesh smoothing seconds: 4.525 Improving mesh... Mesh improvement seconds: 0.159 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.038 Total running seconds: 9.913 Statistics: Input points: 14142 Input facets: 28272 Input segments: 42408 Input holes: 2 Input regions: 0 Mesh points: 32812 Mesh tetrahedra: 158131 Mesh faces: 330398 Mesh faces on exterior boundary: 28272 Mesh faces on input facets: 28272 Mesh edges on input segments: 42408 Steiner points inside domain: 18670 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 1 file(s) copied. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\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 1 file(s) copied. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\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 "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\ESP\venv\Lib\site-packages\f90nml\parser.py", line 378, in _readstream self._update_tokens() File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\ESP\venv\Lib\site-packages\f90nml\parser.py", line 797, in _update_tokens next_token = next(self.tokens) ^^^^^^^^^^^^^^^^^ StopIteration During handling of the above exception, another exception occurred: Traceback (most recent call last): File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\ESP\venv\Lib\site-packages\f90nml\__init__.py", line 31, in read return parser.read(nml_path) ^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\ESP\venv\Lib\site-packages\f90nml\parser.py", line 281, in read return self._readstream(nml_file, nml_patch) ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ File "C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\ESP\venv\Lib\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 1 file(s) copied. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\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. 1 file(s) copied. Writing MAPBC file .... Finished writing MAPBC file Using Python to write FUN3D namelist (fun3d.nml) Reading C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\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! 1 file(s) copied. 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! 1 file(s) copied. 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! 1 file(s) copied. 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 1 file(s) copied. Writing MAPBC file .... Finished writing MAPBC file Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!! Info: No recognized data transfer names found. Reading rubber.data .Closing fun3d!!!! No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Face 3 TFI quading disabled with attribute .qParams Face 6 TFI quading disabled with attribute .qParams Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 4009 Number of elements = 6570 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 5126 Elemental Quad4 = 1444 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 2 Name = box1, index = 1 Name = box2, index = 2 Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 2168 Number of elements = 2166 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 2166 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 2 Property name - box1 Property name - box2 Done getting FEA properties Updating mesh element types based on properties input .No analysis directory provided - defaulting to altName Mapping Csys attributes ................ Number of unique Csys attributes = 0 Getting FEA coordinate systems....... Number of coordinate systems - 0 No coordinate systems found - defaulting to global Mapping capsConstraint attributes ................ Number of unique capsConstraint attributes = 0 Mapping capsLoad attributes ................ Number of unique capsLoad attributes = 0 Mapping capsBound attributes ................ Number of unique capsBound attributes = 0 Mapping capsConnect attributes ................ Number of unique capsConnect attributes = 0 Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 1 Name = box1, index = 1 Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value Setting FEA Data Mesh for body = 0 Number of nodal coordinates = 400 Number of elements = 361 Elemental Nodes = 0 Elemental Rods = 0 Elemental Tria3 = 0 Elemental Quad4 = 361 Getting FEA materials....... Number of materials - 2 Material name - madeupium Material name - unobtainium Done getting FEA materials Getting FEA properties....... Number of properties - 1 Property name - box1 Done getting FEA properties Updating mesh element types based on properties input .ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close! Mapping capsGroup attributes ................ Number of unique capsGroup attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Mapping capsMesh attributes ................ Number of unique capsMesh attributes = 3 Name = Wing1, index = 1 Name = Wing2, index = 2 Name = Farfield, index = 3 Getting mesh sizing parameters Mesh sizing name - Farfield Done getting mesh sizing parameters Getting surface mesh for body 1 (of 3) Getting surface mesh for body 2 (of 3) Getting surface mesh for body 3 (of 3) Body 1 (of 3) Number of nodes = 7750 Number of elements = 15496 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 15496 Number of quadrilateral elements = 0 Body 2 (of 3) Number of nodes = 5870 Number of elements = 11736 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 11736 Number of quadrilateral elements = 0 Body 3 (of 3) Number of nodes = 522 Number of elements = 1040 Number of node elements = 0 Number of line elements = 0 Number of triangle elements = 1040 Number of quadrilateral elements = 0 ---------------------------- Total number of nodes = 14142 Total number of elements = 28272 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 - 14142, elements - 28272 Getting volume mesh Generating volume mesh using TetGen..... Tetgen input string = pYq1.500/0.000T1.00e-16A Delaunizing vertices... Delaunay seconds: 0.342 Creating surface mesh ... Surface mesh seconds: 0.077 Recovering boundaries... Boundary recovery seconds: 0.211 Removing exterior tetrahedra ... Spreading region attributes. Exterior tets removal seconds: 0.128 Recovering Delaunayness... Delaunay recovery seconds: 0.111 Refining mesh... 18851 insertions, added 13350 points, 706982 tetrahedra in queue. 6277 insertions, added 2016 points, 692557 tetrahedra in queue. 8367 insertions, added 2428 points, 526276 tetrahedra in queue. Refinement seconds: 4.411 Smoothing vertices... Mesh smoothing seconds: 4.884 Improving mesh... Mesh improvement seconds: 0.202 Writing nodes. Writing elements. Writing faces. Writing edges. Output seconds: 0.04 Total running seconds: 10.408 Statistics: Input points: 14142 Input facets: 28272 Input segments: 42408 Input holes: 2 Input regions: 0 Mesh points: 32812 Mesh tetrahedra: 158131 Mesh faces: 330398 Mesh faces on exterior boundary: 28272 Mesh faces on input facets: 28272 Mesh edges on input segments: 42408 Steiner points inside domain: 18670 Done meshing using TetGen! Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_1 will be used! Writing SU2 file .... Finished writing SU2 file Getting CFD boundary conditions Boundary condition name - Wing1 . Analysis object with the name, su2AIM, has already been initilized An altName of su2AIM_2 will be used! Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - X .Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " Getting CFD boundary conditions Boundary condition name - Farfield Boundary condition name - Wing1 Boundary condition name - Wing2 Done getting CFD boundary conditions Warning: The su2 cfg file will be overwritten! Write SU2 configuration file for version "Harrier (8.0.0) " . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL Running xFoil...... Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL . ---------------------------------------------------------------------- Ran 67 tests in 174.629s OK (skipped=12) WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'! WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'! WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'! WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'! WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'! WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'! cd ..\..\.. (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\CAPS>set /a "err=0+0+0+0" (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\CAPS>exit /b 0 (venv) C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019\CAPS\aim\skeleton>exit 0 [GNU C Compiler (gcc)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [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: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Successfully parsed console log [Clang] -> found 0 issues (skipped 0 duplicates) [Clang] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [Clang] Skipping post processing [Clang] No filter has been set, publishing all 0 issues [Clang] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Successfully parsed console log [Static Analysis] -> found 0 issues (skipped 0 duplicates) [Static Analysis] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_RegCaps\7.8\CAPS\unit\WIN64.2019') [Static Analysis] Skipping post processing [Static Analysis] No filter has been set, publishing all 0 issues [Static Analysis] Repository miner is not configured, skipping repository mining [Static Analysis] Reference build recorder is not configured [Static Analysis] No valid reference build found [Static Analysis] All reported issues will be considered outstanding [Static Analysis] No quality gates have been set - skipping [Static Analysis] Health report is disabled - skipping [Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues) [Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.8,ESPTEST=CAPS/unit,ESP_ARCH=WIN64.2019,buildnode=windows10x64 #627'. [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