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EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.22
EGADS : OpenCASCADE Version 7.6.0
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 : 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 IER ER Scale Neighbor
EGADS : ID Active ID Flag Weight Factor Faces
EGADS : 1 Yes 0 1 0 1 2
EGADS : 2 Yes 0 1 0 1 1 3
EGADS : 3 Yes 0 1 0 1 2
EGADS : 4 Yes 1 1 NA NA 6 7 8 9
EGADS : 5 Yes 1 1 NA NA 6 7 8 9
EGADS : 6 Yes 1 1 NA NA 4 5 8 9
EGADS : 7 Yes 1 1 NA NA 4 5 8 9
EGADS : 8 Yes 1 1 NA NA 4 5 6 7
EGADS : 9 Yes 1 1 NA NA 4 5 6 7
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1
EGADS : 2 1 3 -2 -3
EGADS : 3 2
EGADS : 4 4 5 -6 -7
EGADS : 5 -8 11 10 -9
EGADS : 6 12 8 -13 -4
EGADS : 7 -14 6 15 -10
EGADS : 8 7 14 -11 -12
EGADS : 9 -5 13 9 -15
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1
EGADS : 2 Yes 1 1 3 -2 -3
EGADS : 3 Yes 1 2
EGADS : 4 Yes 1 4 5 -6 -7
EGADS : 5 Yes 1 -8 11 10 -9
EGADS : 6 Yes 1 12 8 -13 -4
EGADS : 7 Yes 1 -14 6 15 -10
EGADS : 8 Yes 1 7 14 -11 -12
EGADS : 9 Yes 1 -5 13 9 -15
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 1 1 1 2
EGADS : 2 0 Yes 2 2 1 2 3
EGADS : 3 0 Yes 1 2 1 2 2
EGADS : 4 1 Yes 4 3 NA 4 6
EGADS : 5 1 Yes 3 5 NA 4 9
EGADS : 6 1 Yes 6 5 NA 4 7
EGADS : 7 1 Yes 4 6 NA 4 8
EGADS : 8 1 Yes 8 7 NA 5 6
EGADS : 9 1 Yes 7 9 NA 5 9
EGADS : 10 1 Yes 10 9 NA 5 7
EGADS : 11 1 Yes 8 10 NA 5 8
EGADS : 12 1 Yes 4 8 NA 6 8
EGADS : 13 1 Yes 3 7 NA 6 9
EGADS : 14 1 Yes 6 10 NA 7 8
EGADS : 15 1 Yes 5 9 NA 7 9
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 2 0 0.5
EGADS : 2 Yes 3 0 0.5
EGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
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, Faces = 103 173
AFLR4 : Nodes, Faces = 106 179
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 388 692
AFLR4 : Nodes, Faces = 388 692
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 105 177
AFLR4 : Nodes, Faces = 105 177
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1746 3484 512
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1746 3484
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 111 188
AFLR4 : Nodes, Faces = 107 180
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 399 713
AFLR4 : Nodes, Faces = 402 719
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 105 177
AFLR4 : Nodes, Faces = 108 183
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 91 148
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 313 548
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 315 552
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1763 3518 514
OVERALL : CPU Time = 0.061 seconds
Body 1 (of 2)
Number of nodes = 543
Number of elements = 1082
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1082
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1763
Total number of elements = 3518
.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 1.22
EGADS : OpenCASCADE Version 7.6.0
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 : 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 IER ER Scale Neighbor
EGADS : ID Active ID Flag Weight Factor Faces
EGADS : 1 Yes 0 1 NA NA 2 3 4 5
EGADS : 2 Yes 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 1 0 1 7 8 10
EGADS : 12 Yes 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 5 6 -7 -1
EGADS : 3 Yes 1 -2 7 9 -8
EGADS : 4 Yes 1 -10 3 8 -11
EGADS : 5 Yes 1 4 10 -12 -5
EGADS : 6 Yes 1 -6 12 11 -9
EGADS : 7 Yes 1 -13 14 15 -16
EGADS : 8 Yes 1 -17 18 13 -19
EGADS : 9 Yes 1 20 22 -21 -14
EGADS : 10 Yes 1 -15 23 17 -24
EGADS : 11 Yes 1 16 24 19
EGADS : 12 Yes 1 25 26 -20 -18
EGADS : 13 Yes 1 21 27 -25 -23
EGADS : 14 Yes 1 -22 -26 -27
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 NA 1 2
EGADS : 2 0 Yes 1 3 NA 1 3
EGADS : 3 0 Yes 4 3 NA 1 4
EGADS : 4 0 Yes 2 4 NA 1 5
EGADS : 5 0 Yes 2 5 NA 2 5
EGADS : 6 0 Yes 5 6 NA 2 6
EGADS : 7 0 Yes 1 6 NA 2 3
EGADS : 8 0 Yes 3 7 NA 3 4
EGADS : 9 0 Yes 6 7 NA 3 6
EGADS : 10 0 Yes 4 8 NA 4 5
EGADS : 11 0 Yes 8 7 NA 4 6
EGADS : 12 0 Yes 5 8 NA 5 6
EGADS : 13 0 Yes 9 10 1 7 8
EGADS : 14 0 Yes 9 11 1 7 9
EGADS : 15 0 Yes 11 12 1 7 10
EGADS : 16 0 Yes 10 12 1 7 11
EGADS : 17 0 Yes 13 14 1 8 10
EGADS : 18 0 Yes 13 9 1 8 12
EGADS : 19 0 Yes 14 10 1 8 11
EGADS : 20 0 Yes 9 15 1 9 12
EGADS : 21 0 Yes 11 16 1 9 13
EGADS : 22 0 Yes 15 16 1 9 14
EGADS : 23 0 Yes 11 13 1 10 13
EGADS : 24 0 Yes 12 14 1 10 11
EGADS : 25 0 Yes 13 17 1 12 13
EGADS : 26 0 Yes 17 15 1 12 14
EGADS : 27 0 Yes 16 17 1 13 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 40
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 40 40
EGADS : 4 Yes 0 40 0
EGADS : 5 Yes 40 0 0
EGADS : 6 Yes 40 0 40
EGADS : 7 Yes 40 40 40
EGADS : 8 Yes 40 40 0
EGADS : 9 Yes 3.77246052 0 0.00459131419
EGADS : 10 Yes 5.90487498 7.07106781 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 4.0824829 7.07106781 0.123425948
EGADS : 13 Yes 3.77001182 0 0
EGADS : 14 Yes 5.90282524 7.07106781 0
EGADS : 15 Yes 5.90487498 0 0
EGADS : 16 Yes 4.0824829 0 0.123425948
EGADS : 17 Yes 5.90282524 0 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 80
AFLR4 : Min Bounding Box Length = 80
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 2.82843
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 7.60986
AFLR4 : Abs Min Surf Spacing = 0.00707107
AFLR4 : Min Surf Spacing = 0.0141421
AFLR4 : Max Surf Spacing = 0.282843
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 FARFIELD
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 17046 33362
AFLR4 : Nodes, Faces = 7498 14266
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 182 241
AFLR4 : Nodes, Faces = 122 121
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 17145 33560
AFLR4 : Nodes, Faces = 7533 14336
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 14987 29245
AFLR4 : Nodes, Faces = 6850 12971
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 330 546
AFLR4 : Nodes, Faces = 325 536
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 182 241
AFLR4 : Nodes, Faces = 122 121
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 14793 28857
AFLR4 : Nodes, Faces = 6800 12871
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 328 542
AFLR4 : Nodes, Faces = 325 536
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 28549 57090 3616
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 28549 57090
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 137 232
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 137 232
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 14882 29036
AFLR4 : Nodes, Faces = 9506 18284
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 253 368
AFLR4 : Nodes, Faces = 136 134
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 14891 29054
AFLR4 : Nodes, Faces = 9572 18416
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 14110 27494
AFLR4 : Nodes, Faces = 9289 17852
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 348 581
AFLR4 : Nodes, Faces = 370 625
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 253 368
AFLR4 : Nodes, Faces = 136 134
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 13948 27170
AFLR4 : Nodes, Faces = 9375 18024
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 343 571
AFLR4 : Nodes, Faces = 369 623
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 37716 75424 3638
OVERALL : CPU Time = 1.885 seconds
Body 1 (of 1)
Number of nodes = 37716
Number of elements = 75424
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 75424
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 37716
Total number of elements = 75424
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.22
EGADS : OpenCASCADE Version 7.6.0
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 : 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 IER ER Scale Neighbor
EGADS : ID Active ID Flag Weight Factor Faces
EGADS : 1 Yes 0 1 NA NA 2 3 4 5
EGADS : 2 Yes 0 1 NA NA 1 3 5 6
EGADS : 3 Yes 0 1 NA NA 1 2 4 6
EGADS : 4 Yes 0 1 NA NA 1 3 5 6
EGADS : 5 Yes 0 1 NA NA 1 2 4 6
EGADS : 6 Yes 0 1 NA NA 2 3 4 5
EGADS : 7 Yes 0 1 0 1 8 9 10 11
EGADS : 8 Yes 0 1 0 1 7 10 11 12
EGADS : 9 Yes 0 1 0 1 7 12 13 14
EGADS : 10 Yes 0 1 0 1 7 8 11 13
EGADS : 11 Yes 0 1 0 1 7 8 10
EGADS : 12 Yes 0 1 0 1 8 9 13 14
EGADS : 13 Yes 0 1 0 1 9 10 12 14
EGADS : 14 Yes 0 1 0 1 9 12 13
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 5 6 -7 -1
EGADS : 3 -2 7 9 -8
EGADS : 4 -10 3 8 -11
EGADS : 5 4 10 -12 -5
EGADS : 6 -6 12 11 -9
EGADS : 7 -13 14 15 -16
EGADS : 8 -17 18 13 -19
EGADS : 9 20 22 -21 -14
EGADS : 10 -15 23 17 -24
EGADS : 11 16 24 19
EGADS : 12 25 26 -20 -18
EGADS : 13 21 27 -25 -23
EGADS : 14 -22 -26 -27
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 5 6 -7 -1
EGADS : 3 Yes 1 -2 7 9 -8
EGADS : 4 Yes 1 -10 3 8 -11
EGADS : 5 Yes 1 4 10 -12 -5
EGADS : 6 Yes 1 -6 12 11 -9
EGADS : 7 Yes 1 -13 14 15 -16
EGADS : 8 Yes 1 -17 18 13 -19
EGADS : 9 Yes 1 20 22 -21 -14
EGADS : 10 Yes 1 -15 23 17 -24
EGADS : 11 Yes 1 16 24 19
EGADS : 12 Yes 1 25 26 -20 -18
EGADS : 13 Yes 1 21 27 -25 -23
EGADS : 14 Yes 1 -22 -26 -27
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 2 1 NA 1 2
EGADS : 2 0 Yes 1 3 NA 1 3
EGADS : 3 0 Yes 4 3 NA 1 4
EGADS : 4 0 Yes 2 4 NA 1 5
EGADS : 5 0 Yes 2 5 NA 2 5
EGADS : 6 0 Yes 5 6 NA 2 6
EGADS : 7 0 Yes 1 6 NA 2 3
EGADS : 8 0 Yes 3 7 NA 3 4
EGADS : 9 0 Yes 6 7 NA 3 6
EGADS : 10 0 Yes 4 8 NA 4 5
EGADS : 11 0 Yes 8 7 NA 4 6
EGADS : 12 0 Yes 5 8 NA 5 6
EGADS : 13 0 Yes 9 10 1 7 8
EGADS : 14 0 Yes 9 11 1 7 9
EGADS : 15 0 Yes 11 12 1 7 10
EGADS : 16 0 Yes 10 12 1 7 11
EGADS : 17 0 Yes 13 14 1 8 10
EGADS : 18 0 Yes 13 9 1 8 12
EGADS : 19 0 Yes 14 10 1 8 11
EGADS : 20 0 Yes 9 15 1 9 12
EGADS : 21 0 Yes 11 16 1 9 13
EGADS : 22 0 Yes 15 16 1 9 14
EGADS : 23 0 Yes 11 13 1 10 13
EGADS : 24 0 Yes 12 14 1 10 11
EGADS : 25 0 Yes 13 17 1 12 13
EGADS : 26 0 Yes 17 15 1 12 14
EGADS : 27 0 Yes 16 17 1 13 14
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 40
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 40 40
EGADS : 4 Yes 0 40 0
EGADS : 5 Yes 40 0 0
EGADS : 6 Yes 40 0 40
EGADS : 7 Yes 40 40 40
EGADS : 8 Yes 40 40 0
EGADS : 9 Yes 3.77246052 0 0.00459131419
EGADS : 10 Yes 5.90487498 7.07106781 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 4.0824829 7.07106781 0.123425948
EGADS : 13 Yes 3.77001182 0 0
EGADS : 14 Yes 5.90282524 7.07106781 0
EGADS : 15 Yes 5.90487498 0 0
EGADS : 16 Yes 4.0824829 0 0.123425948
EGADS : 17 Yes 5.90282524 0 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 80
AFLR4 : Min Bounding Box Length = 80
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 5.65685
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 7.62074
AFLR4 : Abs Min Surf Spacing = 0.0141421
AFLR4 : Min Surf Spacing = 0.0282843
AFLR4 : Max Surf Spacing = 0.565685
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 FARFIELD
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 6411 12401
AFLR4 : Nodes, Faces = 3199 5977
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 192 273
AFLR4 : Nodes, Faces = 110 109
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 6519 12617
AFLR4 : Nodes, Faces = 3209 5997
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 5814 11207
AFLR4 : Nodes, Faces = 3024 5627
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 257 412
AFLR4 : Nodes, Faces = 258 414
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 192 273
AFLR4 : Nodes, Faces = 110 109
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 5862 11303
AFLR4 : Nodes, Faces = 3013 5605
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 258 414
AFLR4 : Nodes, Faces = 258 414
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 12796 25584 2334
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 12796 25584
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 137 232
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 137 232
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 136 230
AFLR4 : Nodes, Faces = 132 222
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 5943 11465
AFLR4 : Nodes, Faces = 4637 8853
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 226 328
AFLR4 : Nodes, Faces = 122 120
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Faces = 5942 11463
AFLR4 : Nodes, Faces = 4689 8957
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Faces = 5803 11186
AFLR4 : Nodes, Faces = 4470 8520
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Faces = 265 428
AFLR4 : Nodes, Faces = 281 460
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Faces = 226 328
AFLR4 : Nodes, Faces = 122 120
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Faces = 5865 11310
AFLR4 : Nodes, Faces = 4488 8556
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Faces = 265 428
AFLR4 : Nodes, Faces = 281 460
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 18693 37378 2358
OVERALL : CPU Time = 0.795 seconds
Body 1 (of 1)
Number of nodes = 18693
Number of elements = 37378
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 37378
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 18693
Total number of elements = 37378
. 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 1.22
EGADS : OpenCASCADE Version 7.6.0
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 : 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 IER ER Scale Neighbor
EGADS : ID Active ID Flag Weight Factor Faces
EGADS : 1 Yes 0 1 0 1 2
EGADS : 2 Yes 0 1 0 1 1
EGADS : 3 Yes 1 1 NA NA 5 6 7 8
EGADS : 4 Yes 1 1 NA NA 5 6 7 8
EGADS : 5 Yes 1 1 NA NA 3 4 7 8
EGADS : 6 Yes 1 1 NA NA 3 4 7 8
EGADS : 7 Yes 1 1 NA NA 3 4 5 6
EGADS : 8 Yes 1 1 NA NA 3 4 5 6
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 -2 3 4
EGADS : 2 -5 -4 6 2
EGADS : 3 7 8 -9 -10
EGADS : 4 -11 14 13 -12
EGADS : 5 15 11 -16 -7
EGADS : 6 -17 9 18 -13
EGADS : 7 10 17 -14 -15
EGADS : 8 -8 16 12 -18
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 -2 3 4
EGADS : 2 Yes 1 -5 -4 6 2
EGADS : 3 Yes 1 7 8 -9 -10
EGADS : 4 Yes 1 -11 14 13 -12
EGADS : 5 Yes 1 15 11 -16 -7
EGADS : 6 Yes 1 -17 9 18 -13
EGADS : 7 Yes 1 10 17 -14 -15
EGADS : 8 Yes 1 -8 16 12 -18
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Degen 1 1 - 1
EGADS : 2 0 Yes 2 1 1 1 2
EGADS : 3 0 Degen 2 2 - 1
EGADS : 4 0 Yes 2 1 1 1 2
EGADS : 5 0 Degen 1 1 - 2
EGADS : 6 0 Degen 2 2 - 2
EGADS : 7 1 Yes 4 3 NA 3 5
EGADS : 8 1 Yes 3 5 NA 3 8
EGADS : 9 1 Yes 6 5 NA 3 6
EGADS : 10 1 Yes 4 6 NA 3 7
EGADS : 11 1 Yes 8 7 NA 4 5
EGADS : 12 1 Yes 7 9 NA 4 8
EGADS : 13 1 Yes 10 9 NA 4 6
EGADS : 14 1 Yes 8 10 NA 4 7
EGADS : 15 1 Yes 4 8 NA 5 7
EGADS : 16 1 Yes 3 7 NA 5 8
EGADS : 17 1 Yes 6 10 NA 6 7
EGADS : 18 1 Yes 5 9 NA 6 8
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 8.5 0 0.5
EGADS : 2 Yes 8.5 0 0
EGADS : 3 Yes 0 0 2
EGADS : 4 Yes 0 0 0
EGADS : 5 Yes 0 2 2
EGADS : 6 Yes 0 2 0
EGADS : 7 Yes 14 0 2
EGADS : 8 Yes 14 0 0
EGADS : 9 Yes 14 2 2
EGADS : 10 Yes 14 2 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 1
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : 8 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 94 154
AFLR4 : Nodes, Faces = 201 368
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 94 154
AFLR4 : Nodes, Faces = 200 366
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1589 3170 432
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1589 3170
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 81 130
AFLR4 : Nodes, Faces = 204 376
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 79 126
AFLR4 : Nodes, Faces = 203 374
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 91 148
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 313 548
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Faces = 315 552
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1597 3186 428
OVERALL : CPU Time = 0.051 seconds
Body 1 (of 2)
Number of nodes = 377
Number of elements = 750
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 750
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1597
Total number of elements = 3186
.
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 1.22
EGADS : OpenCASCADE Version 7.6.0
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 : 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 IER ER Scale Neighbor
EGADS : ID Active ID Flag Weight Factor Faces
EGADS : 1 Yes 0 1 0 1
EGADS : 2 Yes 1 1 NA NA 4 5 6 7
EGADS : 3 Yes 1 1 NA NA 4 5 6 7
EGADS : 4 Yes 1 1 NA NA 2 3 6 7
EGADS : 5 Yes 1 1 NA NA 2 3 6 7
EGADS : 6 Yes 1 1 NA NA 2 3 4 5
EGADS : 7 Yes 1 1 NA NA 2 3 4 5
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 1 -2
EGADS : 2 3 4 -5 -6
EGADS : 3 -7 10 9 -8
EGADS : 4 11 7 -12 -3
EGADS : 5 -13 5 14 -9
EGADS : 6 6 13 -10 -11
EGADS : 7 -4 12 8 -14
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 -1 2 1 -2
EGADS : 2 Yes 1 3 4 -5 -6
EGADS : 3 Yes 1 -7 10 9 -8
EGADS : 4 Yes 1 11 7 -12 -3
EGADS : 5 Yes 1 -13 5 14 -9
EGADS : 6 Yes 1 6 13 -10 -11
EGADS : 7 Yes 1 -4 12 8 -14
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 1 1 1 1
EGADS : 2 0 Yes 1 1 1 1 1
EGADS : 3 1 Yes 3 2 NA 2 4
EGADS : 4 1 Yes 2 4 NA 2 7
EGADS : 5 1 Yes 5 4 NA 2 5
EGADS : 6 1 Yes 3 5 NA 2 6
EGADS : 7 1 Yes 7 6 NA 3 4
EGADS : 8 1 Yes 6 8 NA 3 7
EGADS : 9 1 Yes 9 8 NA 3 5
EGADS : 10 1 Yes 7 9 NA 3 6
EGADS : 11 1 Yes 3 7 NA 4 6
EGADS : 12 1 Yes 2 6 NA 4 7
EGADS : 13 1 Yes 5 9 NA 5 6
EGADS : 14 1 Yes 4 8 NA 5 7
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 7.25 0 0
EGADS : 2 Yes 0 0 2
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 0 2 2
EGADS : 5 Yes 0 2 0
EGADS : 6 Yes 14 0 2
EGADS : 7 Yes 14 0 0
EGADS : 8 Yes 14 2 2
EGADS : 9 Yes 14 2 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 15
AFLR4 : Min Bounding Box Length = 4
AFLR4 : Max Ref Bounding Box Length = 1.5
AFLR4 : Min Ref Bounding Box Length = 0.5
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 0.5
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.1
AFLR4 : Max Surf Spacing = 0.5
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 FARFIELD
AFLR4 : 3 CAD geometry 0 FARFIELD
AFLR4 : 4 CAD geometry 0 FARFIELD
AFLR4 : 5 CAD geometry 0 FARFIELD
AFLR4 : 6 CAD geometry 0 FARFIELD
AFLR4 : 7 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 919 1710
AFLR4 : Nodes, Faces = 639 1150
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 312 546
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 311 544
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1795 3586 494
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 1795 3586
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Faces = 929 1728
AFLR4 : Nodes, Faces = 666 1202
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Faces = 91 148
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Faces = 92 150
AFLR4 : Nodes, Faces = 88 142
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Faces = 314 550
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Faces = 313 548
AFLR4 : Nodes, Faces = 308 538
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Faces = 315 552
AFLR4 : Nodes, Faces = 308 538
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1821 3638 496
OVERALL : CPU Time = 0.098 seconds
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 (of 2)
Number of nodes = 601
Number of elements = 1202
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1202
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1220
Number of elements = 2436
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2436
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1821
Total number of elements = 3638
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Rib_Root, index = 1
Name = Skin, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1
Number of elements = 1
Number of node elements = 1
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 46
Number of elements = 44
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 44
----------------------------
Total number of nodes = 47
Total number of elements = 45
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 1
Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = Rib_Root, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Rib_Root, index = 1
Name = Skin, index = 2
Name = Wing, index = 3
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 46
Number of elements = 44
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 44
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 47
Combined Number of elements = 45
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 44
Getting vortex lattice surface data
VLM surface name - Skin_Top
Done getting vortex lattice surface data
Getting FEA vortex lattice mesh
Surface 1: Number of points found for aero-spline = 3
Surface 2: Number of points found for aero-spline = 6
(Re-)Combining all aerodynamic surfaces into a 'Wing', 'Canard', and/or 'Fin' single surfaces !
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - Rib_Root
No "material" specified for Property tuple Rib_Root, defaulting to an index of 1
Property name - Skin
No "material" specified for Property tuple Skin, defaulting to an index of 1
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribConstraint
No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribSupport
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - Rib_Root
No "groupName" specified for Connection tuple Rib_Root!
Looking for automatic connections from the use of capsConnectLink for Rib_Root
8 automatic connections were made for capsConnect Rib_Root (node id 1)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Trim1
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Writing aeros card
Writing analysis cards
Writing constraint cards--each subcase individually
Writing support cards
Writing material cards
Writing property cards
Writing aeroelastic cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body 1 (of 1)
Number of nodes = 25
Number of elements = 16
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 16
----------------------------
Total number of nodes = 25
Total number of elements = 16
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = plateEdge, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 1
Name = plate, index = 1
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = plate, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 25
Number of elements = 16
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 16
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 1
Material name - Madeupium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - plate
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - edgeConstraint
No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - appliedPressure
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG
Done running Astros!
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Running avl......
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - VTail1
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - VTail2
No "groupName" variable provided or no matches found, going to use tuple name
VLM surface name - Wing
Done getting vortex lattice surface data
Writing surface - VTail1 (ID = 0)
Section 1 of 2 (ID = 1)
Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Wing, index = 1
Name = hTail, index = 2
Name = vTail, index = 3
Name = VTail1, index = 4
Name = VTail2, index = 5
Getting vortex lattice surface data
VLM surface name - Wing
VLM surface name - hTail
VLM surface name - vTail
No "groupName" variable provided or no matches found, going to use tuple name
Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
Section 1 of 4 (ID = 3)
Section 2 of 4 (ID = 2)
Section 3 of 4 (ID = 1)
Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
Section 1 of 3 (ID = 2)
Section 2 of 3 (ID = 1)
Section 3 of 3 (ID = 0)
Writing surface - vTail (ID = 2)
Section 1 of 2 (ID = 0)
Section 2 of 2 (ID = 1)
Running avl......
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 9607
Number of elements = 19210
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19210
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6142
Number of elements = 12280
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 12280
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 104
Number of elements = 204
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 204
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15853
Total number of elements = 31694
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9631
Number of elements = 19254
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19254
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9631
Total number of elements = 19254
.ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:56026)
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)
20330A500 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
20330A500 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
16E2CB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
16E2CB000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 7 (of 8)
Getting surface mesh for body 8 (of 8)
Body 1 (of 8)
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 8)
Number of nodes = 869
Number of elements = 1734
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1734
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes = 1323
Number of elements = 2642
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2642
Number of quadrilateral elements = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 4 (of 8)
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 8)
Number of nodes = 824
Number of elements = 1644
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1644
Number of quadrilateral elements = 0
Body 6 (of 8)
Number of nodes = 1958
Number of elements = 3916
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3916
Number of quadrilateral elements = 0
Body 7 (of 8)
Number of nodes = 945
Number of elements = 1886
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1886
Number of quadrilateral elements = 0
Body 8 (of 8)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 83235
Total number of elements = 166446
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_1 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75268
Total number of elements = 150528
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_2 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
16E2CB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
16E2CB000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
20330A500 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
20330A500 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1958
Number of elements = 3916
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3916
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75688
Total number of elements = 151372
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_3 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 945
Number of elements = 1886
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1886
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74675
Total number of elements = 149342
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_4 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 1323
Number of elements = 2642
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2642
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75053
Total number of elements = 150098
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_5 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 869
Number of elements = 1734
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1734
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74599
Total number of elements = 149190
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9631
Number of elements = 19254
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19254
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9631
Total number of elements = 19254
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 7174
Number of elements = 14340
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 14340
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7174
Total number of elements = 14340
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_6 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 824
Number of elements = 1644
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1644
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74554
Total number of elements = 149100
.
Analysis object with the name, egadsTessAIM, has already been initilized
An altName of egadsTessAIM_7 will be used!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = torus, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 (of 2)
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75778
Total number of elements = 151552
.Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7819
Number of elements = 15634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5894
Number of elements = 11784
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11784
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 516
Number of elements = 1028
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14229
Total number of elements = 28446
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14229, elements - 28446
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.304942
Creating surface mesh ...
Surface mesh seconds: 0.05755
Recovering boundaries...
Boundary recovery seconds: 0.216874
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.068205
Recovering Delaunayness...
Delaunay recovery seconds: 0.111568
Refining mesh...
18967 insertions, added 13672 points, 705072 tetrahedra in queue.
6316 insertions, added 2535 points, 591326 tetrahedra in queue.
8419 insertions, added 1784 points, 85235 tetrahedra in queue.
Refinement seconds: 4.43748
Smoothing vertices...
Mesh smoothing seconds: 4.053
Improving mesh...
Mesh improvement seconds: 0.15793
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.029264
Total running seconds: 9.43754
Statistics:
Input points: 14229
Input facets: 28446
Input segments: 42669
Input holes: 2
Input regions: 0
Mesh points: 32940
Mesh tetrahedra: 158672
Mesh faces: 331567
Mesh faces on exterior boundary: 28446
Mesh faces on input facets: 28446
Mesh edges on input segments: 42669
Steiner points inside domain: 18711
Done meshing using TetGen!
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
Warning: No boundary condition specified for capsGroup Wing2!
Warning: No boundary condition specified for capsGroup Farfield!
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Error: Python error occurred while writing namelist file
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 378, in _readstream
self._update_tokens()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 798, in _update_tokens
next_token = next(self.tokens)
StopIteration
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "fun3dNamelist.pyx", line 103, in fun3dNamelist.fun3d_writeNMLPython
File "fun3dNamelist.pyx", line 65, in fun3dNamelist.read_fun3d_nml
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/__init__.py", line 31, in read
return parser.read(nml_path)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 281, in read
return self._readstream(nml_file, nml_patch)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/venv/lib/python3.9/site-packages/f90nml/parser.py", line 380, in _readstream
raise ValueError(
ValueError: End-of-file before end of namelist group: '&badNamelist'
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found!
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml .....
Appending namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 1
Objective name - LoD
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Reading rubber.data
.Closing fun3d!!!!
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Creating FEA BEM
Face 3 quading disabled with attribute .qParams
Face 6 quading disabled with attribute .qParams
Getting quads for BEM!
capsIgnore attribute found for face - 1!!
Removing unused nodes...
Removed 324 (out of 4009) unused nodes!
Mesh for body = 0
Number of nodal coordinates = 3685
Number of elements = 6209
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5126
Elemental Quad4 = 1083
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 2166
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2166
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Creating FEA BEM
Getting quads for BEM!
Mesh for body = 0
Number of nodal coordinates = 400
Number of elements = 361
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 361
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
.ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7819
Number of elements = 15634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 15634
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5894
Number of elements = 11784
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11784
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 516
Number of elements = 1028
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1028
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14229
Total number of elements = 28446
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14229, elements - 28446
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.351884
Creating surface mesh ...
Surface mesh seconds: 0.056305
Recovering boundaries...
Boundary recovery seconds: 0.224356
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.089761
Recovering Delaunayness...
Delaunay recovery seconds: 0.109609
Refining mesh...
18967 insertions, added 13672 points, 705072 tetrahedra in queue.
6316 insertions, added 2535 points, 591326 tetrahedra in queue.
8419 insertions, added 1784 points, 85235 tetrahedra in queue.
Refinement seconds: 4.39966
Smoothing vertices...
Mesh smoothing seconds: 3.86217
Improving mesh...
Mesh improvement seconds: 0.159251
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.025829
Total running seconds: 9.27958
Statistics:
Input points: 14229
Input facets: 28446
Input segments: 42669
Input holes: 2
Input regions: 0
Mesh points: 32940
Mesh tetrahedra: 158672
Mesh faces: 331567
Mesh faces on exterior boundary: 28446
Mesh faces on input facets: 28446
Mesh edges on input segments: 42669
Steiner points inside domain: 18711
Done meshing using TetGen!
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_1 will be used!
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Wing1
.
Analysis object with the name, su2AIM, has already been initilized
An altName of su2AIM_2 will be used!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
.Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.4.0) "
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.4.0) "
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
.
Running xFoil......
Running xFoil......
.
----------------------------------------------------------------------
Ran 67 tests in 134.799s
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: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
Legacy AIM unit testing done!
(cd test; ./runUnitTest.sh)
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
aimTransferUtil Tests passed!
real 0m0.192s
user 0m0.094s
sys 0m0.011s
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aimTransferUtilTest passed (as expected)
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/miscUtilsTest
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/miscUtilsTest
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7!
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00
Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00
Returning a 'NaN' string.
Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth > 15 not verified
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0
Returning a 'NaN' string.
miscUtils Tests passed!
real 0m0.151s
user 0m0.076s
sys 0m0.012s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/miscUtilsTest passed (as expected)
=============================================
+ expectCSuccess /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.154s
user 0m0.075s
sys 0m0.009s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/vlmUtilsTest passed (as expected)
=============================================
+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm
Root Path = /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/test/aimTest/Scratch
testingAIM/aimInitialize instance = -1 unitSys = (null)!
caps_queryAnalysis = 0 4 3 1
testingAIM/aimInputs instance = -1 index = 1!
in 1: testingAIMin 0
testingAIM/aimInputs instance = -1 index = 2!
in 2: table 0
testingAIM/aimInputs instance = -1 index = 3!
in 3: tessIn 0
testingAIM/aimInputs instance = -1 index = 4!
in 4: meshFile 0
testingAIM/aimOutputs instance = -1 index = 1!
out 1: testingAIMout 0
testingAIM/aimOutputs instance = -1 index = 2!
out 2: tessOut 0
testingAIM/aimOutputs instance = -1 index = 3!
out 3: meshFile 0
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimBackdoor instance = 0: Input String!
Backdoor return string = aimBackdoor Output
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/test/aimTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 1
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
Problem: # Dirty Analyses = 2!
Bound: # Dirty Analyses = 2!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 1!
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = 0, rank = 1, method = 0
0 scalars!
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
After Execute on Parent
Problem: # Dirty Analyses = 1!
Bound: # Dirty Analyses = 1!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
testingAIM/aimCalcOutput instance = 0 index = 2 tessOut 0!
tessPtr = 0
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimDiscr: tname = Interface, instance = 1!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 3 matches Interface!
testingAIM/aimDiscr: ntris = 2108!
testingAIM/aimDiscr: npts = 1113!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 800!
testingAIM/aimDiscr: npts = 447!
testingAIM/aimTransfer name = scalar instance = 0 npts = 447/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.563194e-13
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
Analysis in Bound = Interface
aim_newGeometry = 0!
getDiscr = 0
getDataSet = -303, rank = 0, method = 0
vectors not setup yet!
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
Dirty = 0
Problem: # Dirty Analyses = 0!
Bound: # Dirty Analyses = 0!
Analys0: # Dirty Analyses = 0!
Analys1: # Dirty Analyses = 0!
Body 1 has length units = cm
Body 2 has length units = cm
aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds
ParamName has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 2
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 3
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 6
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null)
ymin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null)
zmin has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null)
zmax has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null)
unused has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 7
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
value (1x3) =
1: Entry1 -> Value1
2: Entry2 -> Value2
3: Entry3 -> Value3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 8
value (0x0) = NULL with len = 0 writer
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 9
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = 0
aim_getDataSet 0 on Interface = -329
value = 12.340000 cm
lazy: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:38 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:38 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 28
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 28
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 12
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 12
value (1x3) =
1: Entry1 -> newValue1
2: Entry2 -> newValue2
3: Entry3 -> newValue3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 13
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:29 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 10
value (0x0) = NULL with len = 0 writer
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 11
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = 0
aim_getDataSet 1 on Interface = -329
value = 12.340000 cm
lazy: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:38 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 6000032a8c80
value = 6000032a8c80 ego
lazy: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:38 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:38 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 28
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 14
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
1113 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
1113 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 26
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 15
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:37 26
1113 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
447 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 23
447 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 25
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:30 25
447 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:29210 jenkins 2022/12/03 15:05:28 0
testingAIM/aimTransfer name = vector instance = 0 npts = 447/3!
447 points, rank=3, units=(null)
1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
8: 14.400000 14.400000 14.400000 14.380647 14.400000 14.381201 14.400000
15: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
22: 14.400000 14.400000 14.390441 14.400000 14.383859 14.400000 14.400000
29: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
36: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
43: 14.385061 14.400000 14.383844 14.400000 14.400000 14.400000 14.400000
50: 14.378338 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
57: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.376664
64: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
78: 14.389247 14.400000 14.400000 14.400000 14.400000 14.382317 14.400000
85: 14.400000 14.400000 14.400000 14.390011 14.400000 14.400000 14.400000
92: 14.400000 14.400000 14.400000 14.400000 14.389865 14.400000 14.389101
99: 14.400000 14.388170 14.400000 14.400000 14.400000 14.400000 14.400000
106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
260: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
344: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
358: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
379: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
386: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
414: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
449: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
456: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
463: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
470: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
491: 14.400000 14.400000 14.400000 14.400000 14.365872 14.400000 14.400000
498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
505: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
512: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
519: 14.400000 14.362939 14.400000 14.362723 14.400000 14.400000 14.400000
526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
540: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
547: 14.368368 14.400000 14.400000 14.400000 14.400000 14.369831 14.400000
554: 14.400000 14.400000 14.400000 14.368625 14.400000 14.362939 14.400000
561: 14.400000 14.366034 14.400000 14.400000 14.400000 14.400000 14.400000
568: 14.356725 14.400000 14.369831 14.369175 14.400000 14.400000 14.400000
575: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
582: 14.400000 14.363748 14.368368 14.400000 14.400000 14.400000 14.400000
589: 14.369831 14.400000 14.359400 14.400000 14.362294 14.400000 14.400000
596: 14.373876 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
603: 14.369217 14.369217 14.400000 14.365681 14.400000 14.369054 14.400000
610: 14.400000 14.400000 14.400000 14.371385 14.368746 14.372230 14.400000
617: 14.375507 14.400000 14.364430 14.374160 14.400000 14.400000 14.400000
624: 14.368708 14.369354 14.400000 14.400000 14.400000 14.400000 14.400000
631: 14.400000 14.400000 14.370154 14.368219 14.400000 14.372237 14.400000
638: 14.400000 14.374425 14.372363 14.400000 14.400000 14.400000 14.400000
645: 14.375986 14.365557 14.368708 14.366781 14.400000 14.369175 14.369354
652: 14.400000 14.373289 14.400000 14.375685 14.374425 14.400000 14.377582
659: 14.400000 14.400000 14.400000 14.366036 14.400000 14.400000 14.400000
666: 14.400000 14.375124 14.400000 14.400000 14.368903 14.368554 14.400000
673: 14.400000 14.371385 14.371385 14.400000 14.400000 14.379372 14.369129
680: 14.374049 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
687: 14.376399 14.400000 14.377760 14.378863 14.374473 14.367809 14.400000
694: 14.400000 14.368784 14.400000 14.371385 14.365916 14.400000 14.373164
701: 14.400000 14.400000 14.372470 14.400000 14.400000 14.400000 14.400000
708: 14.375986 14.379953 14.400000 14.374316 14.377675 14.400000 14.376295
715: 14.400000 14.400000 14.400000 14.368903 14.368784 14.366475 14.400000
722: 14.400000 14.369555 14.400000 14.378687 14.378687 14.378950 14.400000
729: 14.375449 14.376399 14.371320 14.400000 14.400000 14.371351 14.400000
736: 14.400000 14.375126 14.400000 14.400000 14.400000 14.375504 14.368903
743: 14.368513 14.400000 14.400000 14.400000 14.400000 14.379509 14.375124
750: 14.376289 14.374679 14.400000 14.400000 14.400000 14.400000 14.378601
757: 14.400000 14.377087 14.400000 14.375718 14.373640 14.400000 14.400000
764: 14.372001 14.400000 14.400000 14.368903 14.368513 14.400000 14.374568
771: 14.400000 14.375271 14.400000 14.400000 14.400000 14.400000 14.380017
778: 14.400000 14.400000 14.379331 14.400000 14.400000 14.379693 14.400000
785: 14.372552 14.383094 14.375768 14.400000 14.372608 14.378845 14.400000
792: 14.373363 14.368903 14.400000 14.375189 14.378667 14.375797 14.377675
799: 14.400000 14.400000 14.379863 14.373732 14.400000 14.400000 14.400000
806: 14.400000 14.400000 14.375857 14.400000 14.400000 14.400000 14.400000
813: 14.400000 14.400000 14.400000 14.400000 14.376290 14.379509 14.400000
820: 14.400000 14.400000 14.374594 14.400000 14.376305 14.400000 14.373349
827: 14.400000 14.379553 14.379553 14.373363 14.400000 14.377860 14.382471
834: 14.379565 14.400000 14.376493 14.400000 14.400000 14.400000 14.400000
841: 14.378207 14.375251 14.376604 14.400000 14.378626 14.400000 14.400000
848: 14.400000 14.376156 14.377590 14.379497 14.400000 14.375463 14.378358
855: 14.400000 14.380743 14.375541 14.400000 14.373960 14.400000 14.380592
862: 14.379304 14.374686 14.383536 14.400000 14.400000 14.374081 14.400000
869: 14.400000 14.380716 14.379807 14.383716 14.400000 14.383965 14.377272
876: 14.400000 14.379553 14.400000 14.377569 14.400000 14.376445 14.382213
883: 14.400000 14.400000 14.400000 14.400000 14.371271 14.379704 14.400000
890: 14.400000 14.379157 14.400000 14.379112 14.381121 14.380580 14.400000
897: 14.382553 14.400000 14.383382 14.400000 14.381159 14.400000 14.400000
904: 14.385313 14.382398 14.378148 14.381487 14.400000 14.378926 14.380605
911: 14.400000 14.400000 14.382989 14.384339 14.383216 14.380943 14.382553
918: 14.400000 14.375911 14.400000 14.384096 14.379502 14.376270 14.382299
925: 14.400000 14.380605 14.380605 14.383670 14.382868 14.400000 14.380592
932: 14.400000 14.379140 14.400000 14.400000 14.400000 14.400000 14.379453
939: 14.383433 14.382322 14.382931 14.376461 14.385109 14.386913 14.377699
946: 14.384542 14.400000 14.378601 14.387578 14.400000 14.400000 14.400000
953: 14.385467 14.379641 14.381746 14.383298 14.379930 14.400000 14.381446
960: 14.378196 14.400000 14.400000 14.381473 14.400000 14.383687 14.400000
967: 14.400000 14.384788 14.382697 14.379960 14.382187 14.383771 14.400000
974: 14.376286 14.374476 14.383666 14.382626 14.379930 14.384694 14.384795
981: 14.384528 14.385187 14.382443 14.381568 14.384519 14.385991 14.400000
988: 14.381423 14.400000 14.376098 14.383598 14.400000 14.375887 14.382344
995: 14.400000 14.374828 14.400000 14.386850 14.382671 14.380741 14.377878
1002: 14.388595 14.383868 14.385187 14.400000 14.400000 14.386295 14.384522
1009: 14.388515 14.385094 14.381609 14.387263 14.385337 14.386730 14.386730
1016: 14.387884 14.400000 14.376353 14.377969 14.376461 14.384854 14.378940
1023: 14.400000 14.386177 14.385200 14.385210 14.400000 14.400000 14.388399
1030: 14.384905 14.400000 14.400000 14.385855 14.386303 14.386373 14.389777
1037: 14.383001 14.384393 14.387981 14.400000 14.386362 14.400000 14.400000
1044: 14.400000 14.380951 14.382823 14.381293 14.400000 14.400000 14.375959
1051: 14.380629 14.382255 14.388550 14.385775 14.389044 14.386740 14.385318
1058: 14.400000 14.380768 14.387136 14.385083 14.378339 14.379911 14.379022
1065: 14.400000 14.383818 14.400000 14.373220 14.400000 14.387729 14.382944
1072: 14.387356 14.400000 14.390025 14.387727 14.388858 14.400000 14.381247
1079: 14.386362 14.378339 14.400000 14.400000 14.375685 14.381865 14.383342
1086: 14.386098 14.381327 14.386555 14.381954 14.385445 14.383356 14.384112
1093: 14.379911 14.400000 14.383874 14.400000 14.381637 14.391021 14.400000
1100: 14.400000 14.400000 14.400000 14.400000 14.384655 14.400000 14.378251
1107: 14.400000 14.381756 14.383106 14.386337 14.384313 14.383799 14.384686
source getTriangles = 0, nGtris = 2108, nGsegs = 6324, Ds = 0 0
destin getTriangles = 0, nGtris = 800, nGsegs = 2400, Ds = 0 0
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m9.590s
user 0m9.567s
sys 0m0.309s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/autoExec testingAIM.csm
testingAIM/aimInitialize instance = 0 unitSys = m!
testingAIM/aimInputs instance = 0 index = 1!
testingAIM/aimInputs instance = 0 index = 2!
testingAIM/aimInputs instance = 0 index = 3!
testingAIM/aimInputs instance = 0 index = 4!
testingAIM/aimOutputs instance = 0 index = 1!
testingAIM/aimOutputs instance = 0 index = 2!
testingAIM/aimOutputs instance = 0 index = 3!
testingAIM/aimInitialize instance = 1 unitSys = (null)!
testingAIM/aimInputs instance = 1 index = 1!
testingAIM/aimInputs instance = 1 index = 2!
testingAIM/aimInputs instance = 1 index = 3!
testingAIM/aimInputs instance = 1 index = 4!
testingAIM/aimOutputs instance = 1 index = 1!
testingAIM/aimOutputs instance = 1 index = 2!
testingAIM/aimOutputs instance = 1 index = 3!
Intent = child
APath = /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
testingAIM/aimUpdateState instance = 0!
tess is NULL!
testingAIM/aimPreAnalysis instance = 0!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
getDiscr = -303
meshRef = NULL
testingAIM/aimExecute instance = 0!
testingAIM/aimPostAnalysis instance = 0 restart = 0!
testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
testingAIM/aimCalcOutput instance = 0 index = 1 testingAIMout 0!
aim_getDiscr 0 on Interface = -303
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
testingAIM/aimUpdateState instance = 1!
tess is NULL!
testingAIM/aimPreAnalysis instance = 1!
testingAIM/aimPreAnalysis aim_getBounds = 0
aim_newGeometry = 0!
mesh file = /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
symLink = 0
getDiscr = -303
testingAIM/aimExecute instance = 1!
testingAIM/aimPostAnalysis instance = 1 restart = 0!
testingAIM/aimCalcOutput instance = 1 index = 1 testingAIMout 0!
aim_getDiscr 1 on Interface = -303
*** testingAIMout (child) = 12.340000 1 1 ***
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m1.373s
user 0m1.195s
sys 0m0.164s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1/ESP/DARWINM1/test/autoExec testingAIM.csm passed (as expected)
=============================================
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/unit/DARWINM1')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/unit,DARWINM1,viggen)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/unit,ESP_ARCH=DARWINM1,buildnode=viggen #172' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/unit,ESP_ARCH=DARWINM1,buildnode=viggen #173'.
[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
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