Skipping 1,411 KB..
Full LogAFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1523 3038 476
OVERALL : CPU Time = 0.083 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 = 1219
Number of elements = 2434
Number of triangle elements = 2434
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1523
Total number of elements = 3038
.
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 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 Edges
EGADS : 1 Yes -1
EGADS : 2 Yes 1 3 -2 -3
EGADS : 3 Yes 2
EGADS : 4 Yes 4 5 -6 -7
EGADS : 5 Yes -8 11 10 -9
EGADS : 6 Yes 12 8 -13 -4
EGADS : 7 Yes -14 6 15 -10
EGADS : 8 Yes 7 14 -11 -12
EGADS : 9 Yes -5 13 9 -15
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 1 1 1 2
EGADS : 2 0 Yes 2 2 1 2 3
EGADS : 3 0 Yes 1 2 1 2 2
EGADS : 4 1 Yes 4 3 NA 4 6
EGADS : 5 1 Yes 3 5 NA 4 9
EGADS : 6 1 Yes 6 5 NA 4 7
EGADS : 7 1 Yes 4 6 NA 4 8
EGADS : 8 1 Yes 8 7 NA 5 6
EGADS : 9 1 Yes 7 9 NA 5 9
EGADS : 10 1 Yes 10 9 NA 5 7
EGADS : 11 1 Yes 8 10 NA 5 8
EGADS : 12 1 Yes 4 8 NA 6 8
EGADS : 13 1 Yes 3 7 NA 6 9
EGADS : 14 1 Yes 6 10 NA 7 8
EGADS : 15 1 Yes 5 9 NA 7 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 2 0 0.5
EGADS : 2 Yes 3 0 0.5
EGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
AFLR4 : 9 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 103 173 0
AFLR4 : Nodes, Trias,Quads= 100 167 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 105 177 0
AFLR4 : Nodes, Trias,Quads= 103 173 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1737 3466 512
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1737 3466
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 104 175 0
AFLR4 : Nodes, Trias,Quads= 99 165 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 388 692 0
AFLR4 : Nodes, Trias,Quads= 391 698 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Nodes, Trias,Quads= 102 171 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1738 3468 512
OVERALL : CPU Time = 0.100 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 = 1219
Number of elements = 2434
Number of triangle elements = 2434
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1738
Total number of elements = 3468
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 2 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 27 Edges
EGADS : Body 0 has 14 Loops
EGADS : Body 0 has 17 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 0 1 0 1 7 8 10
EGADS : 12 Yes 0 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 3 8 -11
EGADS : 5 Yes 4 10 -12 -5
EGADS : 6 Yes -6 12 11 -9
EGADS : 7 Yes -13 14 15 -16
EGADS : 8 Yes -17 18 13 -19
EGADS : 9 Yes 20 22 -21 -14
EGADS : 10 Yes -15 23 17 -24
EGADS : 11 Yes 16 24 19
EGADS : 12 Yes 25 26 -20 -18
EGADS : 13 Yes 21 27 -25 -23
EGADS : 14 Yes -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= 17058 33386 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= 17154 33578 0
AFLR4 : Nodes, Trias,Quads= 7368 14006 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 14987 29245 0
AFLR4 : Nodes, Trias,Quads= 6879 13029 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 330 546 0
AFLR4 : Nodes, Trias,Quads= 322 530 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 182 241 0
AFLR4 : Nodes, Trias,Quads= 122 121 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 14793 28857 0
AFLR4 : Nodes, Trias,Quads= 6844 12959 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 328 542 0
AFLR4 : Nodes, Trias,Quads= 324 534 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 28462 56916 3616
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 28462 56916
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 136 230 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 137 232 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 15590 30449 0
AFLR4 : Nodes, Trias,Quads= 9447 18163 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 254 370 0
AFLR4 : Nodes, Trias,Quads= 136 134 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 15870 31009 0
AFLR4 : Nodes, Trias,Quads= 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 = 1.762 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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 1 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 2 Shells
EGADS : Body 0 has 14 Faces
EGADS : Body 0 has 27 Edges
EGADS : Body 0 has 14 Loops
EGADS : Body 0 has 17 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 2 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 0 1 0 1 7 8 10
EGADS : 12 Yes 0 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 2 -3 -4
EGADS : 2 Yes 5 6 -7 -1
EGADS : 3 Yes -2 7 9 -8
EGADS : 4 Yes -10 3 8 -11
EGADS : 5 Yes 4 10 -12 -5
EGADS : 6 Yes -6 12 11 -9
EGADS : 7 Yes -13 14 15 -16
EGADS : 8 Yes -17 18 13 -19
EGADS : 9 Yes 20 22 -21 -14
EGADS : 10 Yes -15 23 17 -24
EGADS : 11 Yes 16 24 19
EGADS : 12 Yes 25 26 -20 -18
EGADS : 13 Yes 21 27 -25 -23
EGADS : 14 Yes -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 = 15.2197
AFLR4 : Abs Min Surf Spacing = 0.00707107
AFLR4 : Min Surf Spacing = 0.0141421
AFLR4 : Max Surf Spacing = 0.282843
AFLR4 : Global Scale Factor = 2
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= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 37 52 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6308 12196 0
AFLR4 : Nodes, Trias,Quads= 3150 5880 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= 6486 12552 0
AFLR4 : Nodes, Trias,Quads= 3253 6086 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5848 11277 0
AFLR4 : Nodes, Trias,Quads= 3043 5667 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 250 400 0
AFLR4 : Nodes, Trias,Quads= 245 390 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= 5864 11309 0
AFLR4 : Nodes, Trias,Quads= 3002 5585 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 249 398 0
AFLR4 : Nodes, Trias,Quads= 244 388 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 12267 24526 2204
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 12267 24526
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 41 60 0
AFLR4 : Nodes, Trias,Quads= 36 50 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 6119 11815 0
AFLR4 : Nodes, Trias,Quads= 4216 8009 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= 6177 11933 0
AFLR4 : Nodes, Trias,Quads= 4307 8193 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 5886 11351 0
AFLR4 : Nodes, Trias,Quads= 4129 7837 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 250 401 0
AFLR4 : Nodes, Trias,Quads= 252 405 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 225 326 0
AFLR4 : Nodes, Trias,Quads= 122 120 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5948 11476 0
AFLR4 : Nodes, Trias,Quads= 4168 7916 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 246 394 0
AFLR4 : Nodes, Trias,Quads= 244 390 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 16649 33290 2234
OVERALL : CPU Time = 0.754 seconds
Body 1 (of 1)
Number of nodes = 16649
Number of elements = 33290
Number of triangle elements = 33290
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 16649
Total number of elements = 33290
.. 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 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 2 Faces
EGADS : Body 0 has 6 Edges
EGADS : Body 0 has 2 Loops
EGADS : Body 0 has 2 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1 2
EGADS : 2 Yes 0 0 1 0 1 1
EGADS : 3 Yes 1 0 1 NA NA 5 6 7 8
EGADS : 4 Yes 1 0 1 NA NA 5 6 7 8
EGADS : 5 Yes 1 0 1 NA NA 3 4 7 8
EGADS : 6 Yes 1 0 1 NA NA 3 4 7 8
EGADS : 7 Yes 1 0 1 NA NA 3 4 5 6
EGADS : 8 Yes 1 0 1 NA NA 3 4 5 6
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 -2 3 4
EGADS : 2 -5 -4 6 2
EGADS : 3 7 8 -9 -10
EGADS : 4 -11 14 13 -12
EGADS : 5 15 11 -16 -7
EGADS : 6 -17 9 18 -13
EGADS : 7 10 17 -14 -15
EGADS : 8 -8 16 12 -18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 -2 3 4
EGADS : 2 Yes -5 -4 6 2
EGADS : 3 Yes 7 8 -9 -10
EGADS : 4 Yes -11 14 13 -12
EGADS : 5 Yes 15 11 -16 -7
EGADS : 6 Yes -17 9 18 -13
EGADS : 7 Yes 10 17 -14 -15
EGADS : 8 Yes -8 16 12 -18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 DEGEN 1 1 - 1
EGADS : 2 0 Yes 2 1 1 1 2
EGADS : 3 0 DEGEN 2 2 - 1
EGADS : 4 0 Yes 2 1 1 1 2
EGADS : 5 0 DEGEN 1 1 - 2
EGADS : 6 0 DEGEN 2 2 - 2
EGADS : 7 1 Yes 4 3 NA 3 5
EGADS : 8 1 Yes 3 5 NA 3 8
EGADS : 9 1 Yes 6 5 NA 3 6
EGADS : 10 1 Yes 4 6 NA 3 7
EGADS : 11 1 Yes 8 7 NA 4 5
EGADS : 12 1 Yes 7 9 NA 4 8
EGADS : 13 1 Yes 10 9 NA 4 6
EGADS : 14 1 Yes 8 10 NA 4 7
EGADS : 15 1 Yes 4 8 NA 5 7
EGADS : 16 1 Yes 3 7 NA 5 8
EGADS : 17 1 Yes 6 10 NA 6 7
EGADS : 18 1 Yes 5 9 NA 6 8
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 8.5 0 0.5
EGADS : 2 Yes 8.5 0 0
EGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 94 154 0
AFLR4 : Nodes, Trias,Quads= 202 370 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 94 154 0
AFLR4 : Nodes, Trias,Quads= 201 368 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1590 3172 432
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1590 3172
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 203 374 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 200 368 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1592 3176 428
OVERALL : CPU Time = 0.105 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 = 1219
Number of elements = 2434
Number of triangle elements = 2434
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1592
Total number of elements = 3176
.
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 1 Faces
EGADS : Body 0 has 2 Edges
EGADS : Body 0 has 1 Loops
EGADS : Body 0 has 1 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 0 1
EGADS : 2 Yes 1 0 1 NA NA 4 5 6 7
EGADS : 3 Yes 1 0 1 NA NA 4 5 6 7
EGADS : 4 Yes 1 0 1 NA NA 2 3 6 7
EGADS : 5 Yes 1 0 1 NA NA 2 3 6 7
EGADS : 6 Yes 1 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 1 0 1 NA NA 2 3 4 5
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 1 -2
EGADS : 2 3 4 -5 -6
EGADS : 3 -7 10 9 -8
EGADS : 4 11 7 -12 -3
EGADS : 5 -13 5 14 -9
EGADS : 6 6 13 -10 -11
EGADS : 7 -4 12 8 -14
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 1 -2
EGADS : 2 Yes 3 4 -5 -6
EGADS : 3 Yes -7 10 9 -8
EGADS : 4 Yes 11 7 -12 -3
EGADS : 5 Yes -13 5 14 -9
EGADS : 6 Yes 6 13 -10 -11
EGADS : 7 Yes -4 12 8 -14
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 1 1 1 1
EGADS : 2 0 Yes 1 1 1 1 1
EGADS : 3 1 Yes 3 2 NA 2 4
EGADS : 4 1 Yes 2 4 NA 2 7
EGADS : 5 1 Yes 5 4 NA 2 5
EGADS : 6 1 Yes 3 5 NA 2 6
EGADS : 7 1 Yes 7 6 NA 3 4
EGADS : 8 1 Yes 6 8 NA 3 7
EGADS : 9 1 Yes 9 8 NA 3 5
EGADS : 10 1 Yes 7 9 NA 3 6
EGADS : 11 1 Yes 3 7 NA 4 6
EGADS : 12 1 Yes 2 6 NA 4 7
EGADS : 13 1 Yes 5 9 NA 5 6
EGADS : 14 1 Yes 4 8 NA 5 7
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 7.25 0 0
EGADS : 2 Yes 0 0 2
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 0 2 2
EGADS : 5 Yes 0 2 0
EGADS : 6 Yes 14 0 2
EGADS : 7 Yes 14 0 0
EGADS : 8 Yes 14 2 2
EGADS : 9 Yes 14 2 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1.5
AFLR4 : Min Ref Bounding Box Length = 0.5
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 919 1710 0
AFLR4 : Nodes, Trias,Quads= 675 1222 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 312 546 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 311 544 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1830 3656 494
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1830 3656
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 930 1730 0
AFLR4 : Nodes, Trias,Quads= 728 1326 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 91 148 0
AFLR4 : Nodes, Trias,Quads= 88 142 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 92 150 0
AFLR4 : Nodes, Trias,Quads= 87 140 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 313 548 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 314 550 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1882 3760 496
OVERALL : CPU Time = 0.112 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 = 1219
Number of elements = 2434
Number of triangle elements = 2434
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1882
Total number of elements = 3760
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 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 IEEE_DENORMAL
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 IEEE_DENORMAL
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 IEEE_DENORMAL
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 IEEE_DENORMAL
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 = 9610
Number of elements = 19216
Number of triangle elements = 19216
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6142
Number of elements = 12280
Number of triangle elements = 12280
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 105
Number of elements = 206
Number of triangle elements = 206
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15857
Total number of elements = 31702
.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 = 9605
Number of elements = 19202
Number of triangle elements = 19202
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9605
Total number of elements = 19202
.ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62511)
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)
7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FF8487D9780 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
70000C013000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
70000C013000 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 = 901
Number of elements = 1798
Number of triangle elements = 1798
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes = 1334
Number of elements = 2664
Number of triangle elements = 2664
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 = 824
Number of elements = 1644
Number of triangle elements = 1644
Number of quadrilateral elements = 0
Body 6 (of 8)
Number of nodes = 1958
Number of elements = 3916
Number of triangle elements = 3916
Number of quadrilateral elements = 0
Body 7 (of 8)
Number of nodes = 942
Number of elements = 1880
Number of triangle elements = 1880
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 = 83275
Total number of elements = 166526
.
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)
70000C013000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
70000C013000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FF8487D9780 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1958
Number of elements = 3916
Number of triangle elements = 3916
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 = 75688
Total number of elements = 151372
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 942
Number of elements = 1880
Number of triangle elements = 1880
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 = 74672
Total number of elements = 149336
.
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 = 1334
Number of elements = 2664
Number of triangle elements = 2664
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 = 75064
Total number of elements = 150120
.
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 = 901
Number of elements = 1798
Number of triangle elements = 1798
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 = 74631
Total number of elements = 149254
.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 = 9605
Number of elements = 19202
Number of triangle elements = 19202
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9605
Total number of elements = 19202
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 = 7161
Number of elements = 14314
Number of triangle elements = 14314
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7161
Total number of elements = 14314
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 824
Number of elements = 1644
Number of triangle elements = 1644
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 = 74554
Total number of elements = 149100
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_7 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
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 = 7819
Number of elements = 15634
Number of triangle elements = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 516
Number of elements = 1028
Number of triangle elements = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14224
Total number of elements = 28436
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 - 14224, elements - 28436
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.15958
Creating surface mesh ...
Surface mesh seconds: 0.033335
Recovering boundaries...
Boundary recovery seconds: 0.11097
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.0436
Recovering Delaunayness...
Delaunay recovery seconds: 0.064225
Refining mesh...
18960 insertions, added 14017 points, 701008 tetrahedra in queue.
6313 insertions, added 2494 points, 554976 tetrahedra in queue.
8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds: 2.20269
Smoothing vertices...
Mesh smoothing seconds: 2.18051
Improving mesh...
Mesh improvement seconds: 0.05348
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.015194
Total running seconds: 4.86413
Statistics:
Input points: 14224
Input facets: 28436
Input segments: 42654
Input holes: 2
Input regions: 0
Mesh points: 33058
Mesh tetrahedra: 159464
Mesh faces: 333146
Mesh faces on exterior boundary: 28436
Mesh faces on input facets: 28436
Mesh edges on input segments: 42654
Steiner points inside domain: 18834
Done meshing using TetGen!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/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-3.11.9/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream
self._update_tokens()
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/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-3.11.9/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-3.11.9/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-3.11.9/lib/python3.11/site-packages/f90nml/parser.py", line 380, in _readstream
raise ValueError(
ValueError: End-of-file before end of namelist group: '&badNamelist'
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/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 = 4009
Number of elements = 6570
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5126
Elemental Quad4 = 1444
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 400
Number of elements = 361
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 361
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7819
Number of elements = 15634
Number of triangle elements = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5889
Number of elements = 11774
Number of triangle elements = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 516
Number of elements = 1028
Number of triangle elements = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14224
Total number of elements = 28436
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 - 14224, elements - 28436
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.158069
Creating surface mesh ...
Surface mesh seconds: 0.027833
Recovering boundaries...
Boundary recovery seconds: 0.113702
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.043693
Recovering Delaunayness...
Delaunay recovery seconds: 0.060451
Refining mesh...
18960 insertions, added 14017 points, 701008 tetrahedra in queue.
6313 insertions, added 2494 points, 554976 tetrahedra in queue.
8415 insertions, added 1753 points, 70 tetrahedra in queue.
Refinement seconds: 2.26844
Smoothing vertices...
Mesh smoothing seconds: 2.22736
Improving mesh...
Mesh improvement seconds: 0.057295
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.014751
Total running seconds: 4.97211
Statistics:
Input points: 14224
Input facets: 28436
Input segments: 42654
Input holes: 2
Input regions: 0
Mesh points: 33058
Mesh tetrahedra: 159464
Mesh faces: 333146
Mesh faces on exterior boundary: 28436
Mesh faces on input facets: 28436
Mesh edges on input segments: 42654
Steiner points inside domain: 18834
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......
.
----------------------------------------------------------------------
Ran 67 tests in 85.994s
OK (skipped=10)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
Legacy AIM unit testing done!
(cd test; ./runUnitTest.sh)
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
aimTransferUtil Tests passed!
real 0m2.127s
user 0m0.184s
sys 0m0.014s
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest passed (as expected)
=============================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00
Returning a 'NaN' string.
Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth > 15 not verified
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
miscUtils Tests passed!
real 0m0.493s
user 0m0.170s
sys 0m0.011s
+ set +x
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest passed (as expected)
=============================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.435s
user 0m0.170s
sys 0m0.011s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest passed (as expected)
=============================================
+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm
Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch
testingAIM/aimInitialize instance = -1 unitSys = (null)!
caps_queryAnalysis = 0 4 3 1
testingAIM/aimInputs instance = -1 index = 1!
in 1: testingAIMin 0
testingAIM/aimInputs instance = -1 index = 2!
in 2: table 0
testingAIM/aimInputs instance = -1 index = 3!
in 3: tessIn 0
testingAIM/aimInputs instance = -1 index = 4!
in 4: meshFile 0
testingAIM/aimOutputs instance = -1 index = 1!
out 1: testingAIMout 0
testingAIM/aimOutputs instance = -1 index = 2!
out 2: tessOut 0
testingAIM/aimOutputs instance = -1 index = 3!
out 3: meshFile 0
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimBackdoor instance = 0: Input String!
Backdoor return string = aimBackdoor Output
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 1
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
Problem: # Dirty Analyses = 2!
Bound: # Dirty Analyses = 2!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 1!
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = 0, rank = 1, method = 0
0 scalars!
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
After Execute on Parent
Problem: # Dirty Analyses = 1!
Bound: # Dirty Analyses = 1!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0!
tessPtr = 0
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimDiscr: tname = Interface, instance = 1!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 3 matches Interface!
testingAIM/aimDiscr: ntris = 1962!
testingAIM/aimDiscr: npts = 1040!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 790!
testingAIM/aimDiscr: npts = 442!
testingAIM/aimTransfer name = scalar instance = 0 npts = 442/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 3.844036e-11
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = -303, rank = 0, method = 0
vectors not setup yet!
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
Dirty = 0
Problem: # Dirty Analyses = 0!
Bound: # Dirty Analyses = 0!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
Body 1 has length units = cm
Body 2 has length units = cm
aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds
ParamName has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 2
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 3
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 6
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null)
ymin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null)
zmin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null)
zmax has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null)
unused has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 7
hist: (null) -> Initial Phase
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 1
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 16
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 16
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
value (1x3) =
1: Entry1 -> Value1
2: Entry2 -> Value2
3: Entry3 -> Value3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 8
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 9
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = 0
aim_getDataSet 0 on Interface = -329
value = 12.340000 cm
lazy: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:10 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:10 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 28
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 28
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 10
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 12
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 12
value (1x3) =
1: Entry1 -> newValue1
2: Entry2 -> newValue2
3: Entry3 -> newValue3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 18
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 13
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 10
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 10
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 11
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = 0
aim_getDataSet 1 on Interface = -329
value = 12.340000 cm
lazy: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:10 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 6000001c8480
value = 6000001c8480 ego
lazy: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:10 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:10 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 28
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 14
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
1040 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
1040 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 26
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 15
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:30:09 26
1040 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
442 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 23
442 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 25
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Child Execute
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:53 25
442 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
hist: (null) -> Starting
aimTest macys.mit.edu:64839 jenkins 2024/06/28 02:29:52 0
testingAIM/aimTransfer name = vector instance = 0 npts = 442/3!
442 points, rank=3, units=(null)
1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
8: 14.400000 14.400000 14.400000 14.400000 14.400000 14.381076 14.400000
15: 14.400000 14.385654 14.400000 14.386399 14.400000 14.400000 14.400000
22: 14.400000 14.400000 14.400000 14.383470 14.400000 14.400000 14.400000
29: 14.400000 14.390663 14.400000 14.400000 14.400000 14.400000 14.400000
36: 14.400000 14.400000 14.390526 14.400000 14.400000 14.400000 14.400000
43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
57: 14.400000 14.400000 14.400000 14.400000 14.377038 14.400000 14.377947
64: 14.400000 14.378370 14.400000 14.380439 14.400000 14.400000 14.400000
71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
78: 14.390431 14.400000 14.400000 14.400000 14.391064 14.400000 14.384912
85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.390113 14.400000
92: 14.400000 14.400000 14.400000 14.400000 14.388870 14.400000 14.400000
99: 14.400000 14.400000 14.386035 14.400000 14.384898 14.400000 14.400000
106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
260: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
344: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
358: 14.382997 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
379: 14.400000 14.400000 14.400000 14.356448 14.400000 14.400000 14.400000
386: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
414: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
449: 14.400000 14.360432 14.400000 14.400000 14.400000 14.400000 14.400000
456: 14.400000 14.400000 14.363710 14.400000 14.400000 14.400000 14.400000
463: 14.400000 14.400000 14.364299 14.400000 14.400000 14.400000 14.400000
470: 14.400000 14.400000 14.400000 14.363289 14.400000 14.400000 14.362208
477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
491: 14.400000 14.400000 14.400000 14.365678 14.400000 14.400000 14.400000
498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363289 14.400000
505: 14.400000 14.400000 14.400000 14.361522 14.400000 14.368098 14.400000
512: 14.400000 14.363976 14.400000 14.400000 14.370432 14.400000 14.400000
519: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363968 14.400000
526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
540: 14.400000 14.400000 14.363289 14.400000 14.400000 14.363979 14.366708
547: 14.368597 14.400000 14.400000 14.400000 14.400000 14.367920 14.400000
554: 14.372633 14.400000 14.400000 14.400000 14.400000 14.362154 14.400000
561: 14.400000 14.400000 14.400000 14.400000 14.400000 14.366708 14.400000
568: 14.369034 14.400000 14.369841 14.371226 14.400000 14.400000 14.400000
575: 14.400000 14.400000 14.368408 14.367520 14.400000 14.368432 14.400000
582: 14.400000 14.400000 14.400000 14.366087 14.400000 14.400000 14.369959
589: 14.367920 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
596: 14.369369 14.368144 14.400000 14.400000 14.400000 14.400000 14.400000
603: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
610: 14.367841 14.372775 14.400000 14.400000 14.400000 14.372125 14.378179
617: 14.400000 14.400000 14.400000 14.400000 14.369095 14.400000 14.400000
624: 14.400000 14.400000 14.400000 14.400000 14.400000 14.367920 14.371353
631: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
638: 14.400000 14.400000 14.400000 14.400000 14.377272 14.376093 14.400000
645: 14.372738 14.400000 14.400000 14.370290 14.400000 14.400000 14.400000
652: 14.400000 14.365824 14.376750 14.400000 14.371580 14.368734 14.400000
659: 14.373031 14.400000 14.371453 14.400000 14.376424 14.373411 14.375742
666: 14.379766 14.400000 14.400000 14.372722 14.400000 14.400000 14.372350
673: 14.400000 14.369868 14.400000 14.379928 14.400000 14.400000 14.400000
680: 14.400000 14.400000 14.372894 14.375220 14.400000 14.400000 14.400000
687: 14.400000 14.400000 14.400000 14.379491 14.373945 14.373477 14.373204
694: 14.369160 14.400000 14.400000 14.371245 14.400000 14.370144 14.400000
701: 14.400000 14.367593 14.400000 14.400000 14.400000 14.400000 14.400000
708: 14.377553 14.400000 14.400000 14.372777 14.400000 14.400000 14.400000
715: 14.400000 14.374692 14.400000 14.400000 14.400000 14.373031 14.375837
722: 14.400000 14.400000 14.370074 14.400000 14.380072 14.400000 14.400000
729: 14.400000 14.400000 14.375022 14.372158 14.400000 14.373856 14.380242
736: 14.400000 14.377974 14.400000 14.400000 14.380573 14.400000 14.400000
743: 14.400000 14.400000 14.400000 14.370484 14.372158 14.375910 14.400000
750: 14.381582 14.375912 14.400000 14.400000 14.379288 14.400000 14.373737
757: 14.400000 14.400000 14.400000 14.379729 14.382285 14.378584 14.400000
764: 14.382311 14.400000 14.400000 14.374409 14.371245 14.379232 14.373945
771: 14.400000 14.376341 14.400000 14.400000 14.377043 14.378486 14.374858
778: 14.382054 14.400000 14.383869 14.381636 14.377184 14.400000 14.400000
785: 14.400000 14.372636 14.400000 14.368456 14.383921 14.400000 14.400000
792: 14.383458 14.400000 14.400000 14.400000 14.400000 14.400000 14.381953
799: 14.400000 14.374858 14.373072 14.378348 14.379772 14.400000 14.378216
806: 14.378852 14.400000 14.400000 14.400000 14.380161 14.400000 14.400000
813: 14.384556 14.381516 14.400000 14.376255 14.400000 14.380120 14.400000
820: 14.400000 14.380472 14.379996 14.400000 14.373072 14.400000 14.373126
827: 14.379728 14.388089 14.378410 14.377743 14.383644 14.400000 14.400000
834: 14.381170 14.377592 14.376925 14.384404 14.383167 14.400000 14.382056
841: 14.400000 14.383692 14.400000 14.383013 14.384733 14.400000 14.400000
848: 14.400000 14.380633 14.400000 14.400000 14.400000 14.373808 14.381358
855: 14.400000 14.400000 14.383124 14.400000 14.400000 14.385360 14.376255
862: 14.373590 14.400000 14.383049 14.386052 14.382506 14.381131 14.383698
869: 14.384781 14.379968 14.383657 14.384709 14.377957 14.400000 14.380975
876: 14.400000 14.375227 14.400000 14.379017 14.378731 14.378357 14.376010
883: 14.373652 14.383370 14.383357 14.385444 14.385424 14.381819 14.384645
890: 14.379402 14.389897 14.380433 14.400000 14.383857 14.385410 14.384756
897: 14.379335 14.385835 14.400000 14.385091 14.374477 14.383079 14.383855
904: 14.380149 14.374722 14.383296 14.381983 14.376090 14.383810 14.378363
911: 14.387375 14.383245 14.378412 14.383393 14.382951 14.382465 14.382804
918: 14.384507 14.385472 14.385336 14.385820 14.384140 14.385028 14.385702
925: 14.383042 14.388214 14.388256 14.382050 14.381706 14.379795 14.381159
932: 14.381897 14.378803 14.384372 14.381369 14.386079 14.387357 14.385924
939: 14.382744 14.381612 14.381032 14.386745 14.385849 14.379042 14.385090
946: 14.400000 14.381764 14.381240 14.379650 14.385693 14.385693 14.386153
953: 14.384626 14.387791 14.385449 14.400000 14.385665 14.400000 14.379731
960: 14.380272 14.385409 14.385781 14.381733 14.382438 14.385533 14.380583
967: 14.386516 14.384573 14.400000 14.378382 14.384594 14.400000 14.386153
974: 14.382680 14.389375 14.386802 14.381707 14.379398 14.380377 14.386666
981: 14.387596 14.388630 14.387987 14.379180 14.386395 14.386595 14.400000
988: 14.385128 14.382720 14.381637 14.387158 14.381496 14.389287 14.386767
995: 14.382154 14.388300 14.384113 14.381877 14.390676 14.383198 14.387762
1002: 14.386642 14.388993 14.383485 14.387635 14.390869 14.381952 14.382376
1009: 14.381221 14.379752 14.400000 14.382249 14.378060 14.383886 14.382511
1016: 14.387091 14.386270 14.384482 14.387626 14.381697 14.387252 14.400000
1023: 14.378331 14.384910 14.381021 14.388566 14.400000 14.388325 14.387032
1030: 14.378428 14.387252 14.379752 14.400000 14.384558 14.384911 14.381221
1037: 14.378848 14.384694 14.382523 14.382981
source getTriangles = 0, nGtris = 1962, nGsegs = 5886, Ds = 0 0
destin getTriangles = 0, nGtris = 790, nGsegs = 2370, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m18.726s
user 0m17.270s
sys 0m0.535s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
getDiscr = -303
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = -303
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
mesh file = /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
symLink = 0
getDiscr = -303
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = -303
*** testingAIMout (child) = 12.340000 1 1 ***
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m1.156s
user 0m0.765s
sys 0m0.201s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm passed (as expected)
=============================================
++ set +x
[Execution node] check if [macys] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64')
[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] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/unit/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.7,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys #667'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS