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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= 88 142 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= 311 544 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= 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= 1240 2472 416
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1240 2472
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1240 2472 416
OVERALL : CPU Time = 0.170 seconds
Body 1 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1240
Total number of elements = 2472
.
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1680 3352 494
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1680 3352
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1689 3370 498
OVERALL : CPU Time = 0.240 seconds
Body 1 (of 2)
Number of nodes = 469
Number of elements = 934
Number of triangle elements = 934
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1689
Total number of elements = 3370
.
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1507 3006 476
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1507 3006
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1524 3040 476
OVERALL : CPU Time = 0.143 seconds
Body 1 (of 2)
Number of nodes = 304
Number of elements = 604
Number of triangle elements = 604
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1524
Total number of elements = 3040
.
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1738 3468 512
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1738 3468
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 104 175 0
AFLR4 : Nodes, Trias,Quads= 99 165 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 391 698 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1739 3470 512
OVERALL : CPU Time = 0.098 seconds
Body 1 (of 2)
Number of nodes = 519
Number of elements = 1034
Number of triangle elements = 1034
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1739
Total number of elements = 3470
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
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= 17055 33380 0
AFLR4 : Nodes, Trias,Quads= 7507 14284 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 182 241 0
AFLR4 : Nodes, Trias,Quads= 122 121 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 17164 33598 0
AFLR4 : Nodes, Trias,Quads= 7368 14006 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 14987 29245 0
AFLR4 : Nodes, Trias,Quads= 6879 13029 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 330 546 0
AFLR4 : Nodes, Trias,Quads= 322 530 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 182 241 0
AFLR4 : Nodes, Trias,Quads= 122 121 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 14793 28857 0
AFLR4 : Nodes, Trias,Quads= 6844 12959 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 328 542 0
AFLR4 : Nodes, Trias,Quads= 324 534 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 28462 56916 3616
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 28462 56916
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 15590 30449 0
AFLR4 : Nodes, Trias,Quads= 9447 18163 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 254 370 0
AFLR4 : Nodes, Trias,Quads= 136 134 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 15870 31009 0
AFLR4 : Nodes, Trias,Quads= 9439 18147 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 14689 28649 0
AFLR4 : Nodes, Trias,Quads= 9247 17765 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 346 577 0
AFLR4 : Nodes, Trias,Quads= 359 603 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 254 370 0
AFLR4 : Nodes, Trias,Quads= 136 134 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 14582 28435 0
AFLR4 : Nodes, Trias,Quads= 9309 17889 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 348 581 0
AFLR4 : Nodes, Trias,Quads= 361 607 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 37391 74774 3650
OVERALL : CPU Time = 1.575 seconds
Body 1 (of 1)
Number of nodes = 37391
Number of elements = 74774
Number of triangle elements = 74774
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 37391
Total number of elements = 74774
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 2 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 27 Edges
EGADS : Body 0 has 14 Loops
EGADS : Body 0 has 17 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 0 1 0 1 7 8 10
EGADS : 12 Yes 0 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 5 6 -7 -1
EGADS : 3 Yes 1 -2 7 9 -8
EGADS : 4 Yes 1 -10 3 8 -11
EGADS : 5 Yes 1 4 10 -12 -5
EGADS : 6 Yes 1 -6 12 11 -9
EGADS : 7 Yes 1 -13 14 15 -16
EGADS : 8 Yes 1 -17 18 13 -19
EGADS : 9 Yes 1 20 22 -21 -14
EGADS : 10 Yes 1 -15 23 17 -24
EGADS : 11 Yes 1 16 24 19
EGADS : 12 Yes 1 25 26 -20 -18
EGADS : 13 Yes 1 21 27 -25 -23
EGADS : 14 Yes 1 -22 -26 -27
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 NA 1 2
EGADS : 2 0 Yes 1 3 NA 1 3
EGADS : 3 0 Yes 4 3 NA 1 4
EGADS : 4 0 Yes 2 4 NA 1 5
EGADS : 5 0 Yes 2 5 NA 2 5
EGADS : 6 0 Yes 5 6 NA 2 6
EGADS : 7 0 Yes 1 6 NA 2 3
EGADS : 8 0 Yes 3 7 NA 3 4
EGADS : 9 0 Yes 6 7 NA 3 6
EGADS : 10 0 Yes 4 8 NA 4 5
EGADS : 11 0 Yes 8 7 NA 4 6
EGADS : 12 0 Yes 5 8 NA 5 6
EGADS : 13 0 Yes 9 10 1 7 8
EGADS : 14 0 Yes 9 11 1 7 9
EGADS : 15 0 Yes 11 12 1 7 10
EGADS : 16 0 Yes 10 12 1 7 11
EGADS : 17 0 Yes 13 14 1 8 10
EGADS : 18 0 Yes 13 9 1 8 12
EGADS : 19 0 Yes 14 10 1 8 11
EGADS : 20 0 Yes 9 15 1 9 12
EGADS : 21 0 Yes 11 16 1 9 13
EGADS : 22 0 Yes 15 16 1 9 14
EGADS : 23 0 Yes 11 13 1 10 13
EGADS : 24 0 Yes 12 14 1 10 11
EGADS : 25 0 Yes 13 17 1 12 13
EGADS : 26 0 Yes 17 15 1 12 14
EGADS : 27 0 Yes 16 17 1 13 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 40
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 40 40
EGADS : 4 Yes 0 40 0
EGADS : 5 Yes 40 0 0
EGADS : 6 Yes 40 0 40
EGADS : 7 Yes 40 40 40
EGADS : 8 Yes 40 40 0
EGADS : 9 Yes 3.77246052 0 0.00459131419
EGADS : 10 Yes 5.90487498 7.07106781 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 4.0824829 7.07106781 0.123425948
EGADS : 13 Yes 3.77001182 0 0
EGADS : 14 Yes 5.90282524 7.07106781 0
EGADS : 15 Yes 5.90487498 0 0
EGADS : 16 Yes 4.0824829 0 0.123425948
EGADS : 17 Yes 5.90282524 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 80
AFLR4 : Min Bounding Box Length = 80
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 5.65685
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 7.62074
AFLR4 : Abs Min Surf Spacing = 0.0141421
AFLR4 : Min Surf Spacing = 0.0282843
AFLR4 : Max Surf Spacing = 0.565685
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 FARFIELD
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6411 12401 0
AFLR4 : Nodes, Trias,Quads= 3253 6085 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 192 273 0
AFLR4 : Nodes, Trias,Quads= 110 109 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6519 12617 0
AFLR4 : Nodes, Trias,Quads= 3180 5939 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5814 11207 0
AFLR4 : Nodes, Trias,Quads= 3048 5675 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 257 412 0
AFLR4 : Nodes, Trias,Quads= 256 410 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 192 273 0
AFLR4 : Nodes, Trias,Quads= 110 109 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5862 11303 0
AFLR4 : Nodes, Trias,Quads= 3028 5635 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 258 414 0
AFLR4 : Nodes, Trias,Quads= 256 410 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 12856 25704 2334
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 12856 25704
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6200 11975 0
AFLR4 : Nodes, Trias,Quads= 4633 8841 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 226 328 0
AFLR4 : Nodes, Trias,Quads= 122 120 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 6154 11884 0
AFLR4 : Nodes, Trias,Quads= 4634 8844 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5942 11461 0
AFLR4 : Nodes, Trias,Quads= 4482 8541 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 263 424 0
AFLR4 : Nodes, Trias,Quads= 268 434 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 226 328 0
AFLR4 : Nodes, Trias,Quads= 122 120 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5975 11528 0
AFLR4 : Nodes, Trias,Quads= 4473 8524 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 265 428 0
AFLR4 : Nodes, Trias,Quads= 270 438 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 18601 37194 2370
OVERALL : CPU Time = 0.718 seconds
Body 1 (of 1)
Number of nodes = 18601
Number of elements = 37194
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1591 3174 432
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1591 3174
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 203 374 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 200 368 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1593 3178 428
OVERALL : CPU Time = 0.089 seconds
Body 1 (of 2)
Number of nodes = 373
Number of elements = 742
Number of triangle elements = 742
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1593
Total number of elements = 3178
.
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
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= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1831 3658 494
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1831 3658
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 930 1730 0
AFLR4 : Nodes, Trias,Quads= 728 1326 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 315 552 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1883 3762 496
OVERALL : CPU Time = 0.100 seconds
Body 1 (of 2)
Number of nodes = 663
Number of elements = 1326
Number of triangle elements = 1326
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1883
Total number of elements = 3762
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 44
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Running avl......
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 0)
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Running avl......
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 9573
Number of elements = 19142
Number of triangle elements = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6160
Number of elements = 12316
Number of triangle elements = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 104
Number of elements = 204
Number of triangle elements = 204
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15837
Total number of elements = 31662
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
.ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:61955)
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)
173BBB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
173BBB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 8)
Getting surface mesh for body 8 (of 8)
Body 1 (of 8)
Number of nodes = 1538
Number of elements = 3072
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 8)
Number of nodes = 873
Number of elements = 1742
Number of triangle elements = 1742
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes = 1315
Number of elements = 2626
Number of triangle elements = 2626
Number of quadrilateral elements = 0
Body 4 (of 8)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 8)
Number of nodes = 822
Number of elements = 1640
Number of triangle elements = 1640
Number of quadrilateral elements = 0
Body 6 (of 8)
Number of nodes = 1959
Number of elements = 3918
Number of triangle elements = 3918
Number of quadrilateral elements = 0
Body 7 (of 8)
Number of nodes = 935
Number of elements = 1866
Number of triangle elements = 1866
Number of quadrilateral elements = 0
Body 8 (of 8)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 83220
Total number of elements = 166416
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1538
Number of elements = 3072
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75268
Total number of elements = 150528
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
173BBB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
173BBB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1959
Number of elements = 3918
Number of triangle elements = 3918
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75689
Total number of elements = 151374
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 935
Number of elements = 1866
Number of triangle elements = 1866
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74665
Total number of elements = 149322
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1315
Number of elements = 2626
Number of triangle elements = 2626
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75045
Total number of elements = 150082
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 873
Number of elements = 1742
Number of triangle elements = 1742
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74603
Total number of elements = 149198
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 7151
Number of elements = 14294
Number of triangle elements = 14294
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7151
Total number of elements = 14294
.E EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 822
Number of elements = 1640
Number of triangle elements = 1640
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74552
Total number of elements = 149096
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_7 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75778
Total number of elements = 151552
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.232876
Creating surface mesh ...
Surface mesh seconds: 0.03792
Recovering boundaries...
Boundary recovery seconds: 0.166731
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.05814
Recovering Delaunayness...
Delaunay recovery seconds: 0.067001
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 3.39404
Smoothing vertices...
Mesh smoothing seconds: 2.97155
Improving mesh...
Mesh improvement seconds: 0.088259
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.01721
Total running seconds: 7.03457
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
Done meshing using TetGen!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Error: Python error occurred while writing namelist file
Traceback (most recent call last):
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream
self._update_tokens()
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/python3.11/site-packages/f90nml/parser.py", line 797, in _update_tokens
next_token = next(self.tokens)
^^^^^^^^^^^^^^^^^
StopIteration
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython
File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read
return parser.read(nml_path)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/python3.11/site-packages/f90nml/parser.py", line 281, in read
return self._readstream(nml_file, nml_patch)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.6/lib/python3.11/site-packages/f90nml/parser.py", line 380, in _readstream
raise ValueError(
ValueError: End-of-file before end of namelist group: '&badNamelist'
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 1
Objective name - LoD
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Reading rubber.data
.Closing fun3d!!!!
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Face 3 TFI quading disabled with attribute .qParams
Face 6 TFI quading disabled with attribute .qParams
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 4048
Number of elements = 6648
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5204
Elemental Quad4 = 1444
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 400
Number of elements = 361
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 361
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.207896
Creating surface mesh ...
Surface mesh seconds: 0.044469
Recovering boundaries...
Boundary recovery seconds: 0.160457
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.052476
Recovering Delaunayness...
Delaunay recovery seconds: 0.086244
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 3.65833
Smoothing vertices...
Mesh smoothing seconds: 3.20223
Improving mesh...
Mesh improvement seconds: 0.118603
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.037186
Total running seconds: 7.56861
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
Done meshing using TetGen!
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_1 will be used!
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
Running xFoil......
.
======================================================================
ERROR: test_setAnalysisVals (test_egadsTess.TestEGADS.test_setAnalysisVals)
----------------------------------------------------------------------
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/test_egadsTess.py", line 98, in test_setAnalysisVals
myAnalysis.setAnalysisVal("Multiple_Mesh", True)
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/problem.py", line 63, in wrapper_deprecated
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/problem.py", line 2863, in setAnalysisVal
self.input[varname].value = caps._withUnits(value, units)
^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/problem.py", line 1573, in value
self._valObj.setValue(val)
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 2281, in setValue
_raiseStatus(stat, msg="Trying to set value for: {!r}".format(name), errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_BADTYPE: Trying to set value for: 'Multiple_Mesh':
================================================================================
================================================================================
----------------------------------------------------------------------
Ran 67 tests in 96.036s
FAILED (errors=1, skipped=10)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
make[1]: *** [test] Error 1
make: *** [unitaim] Error 2
++ true
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_MemcheckCaps/CASREV=7.8,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #1381'.
[Checks API] No suitable checks publisher found.
Build step 'Console output (build log) parsing' changed build result to FAILURE
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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