Console Output

Skipping 1,069 KB.. Full Log
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=      1535      3062       476

OVERALL  : CPU Time          =     0.084   seconds
Body 1 (of 2)
Number of nodes    = 315
Number of elements = 626
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 626
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    = 1535
Total number of elements = 3062
.
Analysis object with the name, aflr4AIM, has already been initilized
An altName of aflr4AIM_4 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.4.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 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          =     0.105   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 7.4.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 2 Shells
EGADS    : Body 0 has 14 Faces
EGADS    : Body 0 has 27 Edges
EGADS    : Body 0 has 14 Loops
EGADS    : Body 0 has 17 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : 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      =     17058     33386
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      =     17154     33578
AFLR4    : Nodes, Faces      =      7532     14334

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=     28548     57088      3616

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =     28548     57088

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      =      9503     18278

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      =      9569     18410

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Faces      =     14110     27494
AFLR4    : Nodes, Faces      =      9288     17850

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      =      9376     18026

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=     37710     75412      3638

OVERALL  : CPU Time          =     2.159   seconds
Body 1 (of 1)
Number of nodes    = 37710
Number of elements = 75412
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 75412
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 37710
Total number of elements = 75412

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.4.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 1 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 2 Shells
EGADS    : Body 0 has 14 Faces
EGADS    : Body 0 has 27 Edges
EGADS    : Body 0 has 14 Loops
EGADS    : Body 0 has 17 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : 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      =      4477      8534

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      =      4485      8550

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=     18697     37386      2358

OVERALL  : CPU Time          =     0.819   seconds
Body 1 (of 1)
Number of nodes    = 18697
Number of elements = 37386
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 37386
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 18697
Total number of elements = 37386
.. 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 7.4.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 2 Faces
EGADS    : Body 0 has 6 Edges
EGADS    : Body 0 has 2 Loops
EGADS    : Body 0 has 2 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : 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          =     0.079   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 7.4.1
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 1 Faces
EGADS    : Body 0 has 2 Edges
EGADS    : Body 0 has 1 Loops
EGADS    : Body 0 has 1 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : 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      =       640      1152

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=      1796      3588       494

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      1796      3588

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Faces      =       929      1728
AFLR4    : Nodes, Faces      =       669      1208

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=      1824      3644       496

OVERALL  : CPU Time          =     0.107   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    = 604
Number of elements = 1208
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1208
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    = 1824
Total number of elements = 3644
.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 IEEE_DENORMAL
Done running Astros!
.No analysis directory provided - defaulting to altName
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
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 IEEE_DENORMAL
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 1
	Material name - Madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - plate
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used

Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file

Writing subElement types (if any) - appending mesh file

Writing Astros instruction file....
	Writing analysis cards
	Writing load ADD cards
	Writing constraint cards--each subcase individually
	Writing load cards
	Writing material cards
	Writing property cards


Running Astros......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Done running Astros!
.Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
Writing mass properties file: caps.mass
Parsing MassProp
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_1 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)


Running avl......


Running avl......


Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_2 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)


Running avl......
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)


Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_3 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_4 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - VTail1
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VTail2
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - VTail1 (ID = 0)
	Section 1 of 2 (ID = 1)
	Section 2 of 2 (ID = 0)
Writing surface - VTail2 (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)


Running avl......
.
Analysis object with the name, avlAIM, has already been initilized
An altName of avlAIM_5 will be used!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 2)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 0)
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)


Running avl......
.Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 9618
Number of elements = 19232
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19232
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    = 123
Number of elements = 242
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 242
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 15883
Total number of elements = 31754
.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    = 9601
Number of elements = 19194
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19194
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9601
Total number of elements = 19194
.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)
 70000D91D000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 70000D91D000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 1059EFE00 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 1059EFE00 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    = 906
Number of elements = 1808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1808
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes    = 1332
Number of elements = 2660
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 2660
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    = 946
Number of elements = 1888
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1888
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    = 83282
Total number of elements = 166540
.
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)
 1059EFE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 1059EFE00 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 70000D91D000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 70000D91D000 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    = 946
Number of elements = 1888
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1888
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    = 74676
Total number of elements = 149344
.
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    = 1332
Number of elements = 2660
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 2660
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    = 75062
Total number of elements = 150116
.
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    = 906
Number of elements = 1808
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1808
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    = 74636
Total number of elements = 149264
.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    = 9601
Number of elements = 19194
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 19194
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9601
Total number of elements = 19194
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    = 7173
Number of elements = 14338
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 14338
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 7173
Total number of elements = 14338
. 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    = 7820
Number of elements = 15636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 524
Number of elements = 1044
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14233
Total number of elements = 28454
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 - 14233, elements - 28454
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.469514
Creating surface mesh ...
Surface mesh seconds:  0.061654
Recovering boundaries...
Boundary recovery seconds:  0.367259
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.181461
Recovering Delaunayness...
Delaunay recovery seconds:  0.124514
Refining mesh...
  18972 insertions, added 13254 points, 701278 tetrahedra in queue.
  6317 insertions, added 2883 points, 614952 tetrahedra in queue.
  8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds:  4.13337
Smoothing vertices...
Mesh smoothing seconds:  4.08423
Improving mesh...
Mesh improvement seconds:  0.086328

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.040011
Total running seconds:  9.5495

Statistics:

  Input points: 14233
  Input facets: 28454
  Input segments: 42681
  Input holes: 2
  Input regions: 0

  Mesh points: 33078
  Mesh tetrahedra: 159812
  Mesh faces: 333851
  Mesh faces on exterior boundary: 28454
  Mesh faces on input facets: 28454
  Mesh edges on input segments: 42681
  Steiner points inside domain: 18845

Done meshing using TetGen!

Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_1 will be used!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest4_fun3dAIM/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_2 will be used!
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Traceback (most recent call last):
  File "/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/venv/lib/python3.10/site-packages/f90nml/parser.py", line 378, in _readstream
	Error: Python error occurred while writing namelist file
    self._update_tokens()
  File "/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/venv/lib/python3.10/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_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/venv/lib/python3.10/site-packages/f90nml/__init__.py", line 31, in read
    return parser.read(nml_path)
  File "/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/venv/lib/python3.10/site-packages/f90nml/parser.py", line 281, in read
    return self._readstream(nml_file, nml_patch)
  File "/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/venv/lib/python3.10/site-packages/f90nml/parser.py", line 380, in _readstream
    raise ValueError(
ValueError: End-of-file before end of namelist group: '&badNamelist'
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_3 will be used!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)
	/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml not found!
	Creating namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.

Writing MAPBC file ....
Finished writing MAPBC file


Using Python to write FUN3D namelist (fun3d.nml)

	Reading /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest6_fun3dAIM/fun3d.nml .....
	Appending namelist
	Done writing nml file with Python
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_4 will be used!
Getting CFD boundary conditions
	Boundary condition name - Wing1
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_5 will be used!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_6 will be used!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
.Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
.
Analysis object with the name, fun3dAIM, has already been initilized
An altName of fun3dAIM_7 will be used!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - LoD
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Reading rubber.data 
.Closing fun3d!!!!
No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
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    = 7820
Number of elements = 15636
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 15636
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5889
Number of elements = 11774
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11774
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 524
Number of elements = 1044
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14233
Total number of elements = 28454
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 - 14233, elements - 28454
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.446128
Creating surface mesh ...
Surface mesh seconds:  0.061456
Recovering boundaries...
Boundary recovery seconds:  0.203572
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.090978
Recovering Delaunayness...
Delaunay recovery seconds:  0.099553
Refining mesh...
  18972 insertions, added 13254 points, 701278 tetrahedra in queue.
  6317 insertions, added 2883 points, 614952 tetrahedra in queue.
  8421 insertions, added 2047 points, 103425 tetrahedra in queue.
Refinement seconds:  3.97163
Smoothing vertices...
Mesh smoothing seconds:  3.58705
Improving mesh...
Mesh improvement seconds:  0.09467

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.036444
Total running seconds:  8.59257

Statistics:

  Input points: 14233
  Input facets: 28454
  Input segments: 42681
  Input holes: 2
  Input regions: 0

  Mesh points: 33078
  Mesh tetrahedra: 159812
  Mesh faces: 333851
  Mesh faces on exterior boundary: 28454
  Mesh faces on input facets: 28454
  Mesh edges on input segments: 42681
  Steiner points inside domain: 18845

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......
Note: The following floating-point exceptions are signalling: IEEE_DENORMAL
.
----------------------------------------------------------------------
Ran 67 tests in 117.235s

OK (skipped=10)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.getGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
Legacy AIM unit testing done!
(cd test; ./runUnitTest.sh)
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 84) at Close!
aimTransferUtil Tests passed!

real	0m0.321s
user	0m0.038s
sys	0m0.012s

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aimTransferUtilTest passed (as expected)
=============================================

+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest
+ /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 0.000000E+00
	Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of -2 must be greater than 1 for the input value 9.000000E+00
	Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 0 must be greater than 1 for the input value 9.000000E+00
	Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -1.000000E+100 with field with 7!
	Returning a 'NaN' string.
Error in convert_doubleToString: Cannot write -9.900000E+99 with field with 7!
	Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 2 must be greater than 2 for the input value -1.000000E+00
	Returning a 'NaN' string.
Error in convert_doubleToString: Input fieldWidth of 1 must be greater than 1 for the input value 1.000000E+00
	Returning a 'NaN' string.
Error in convert_integerToString: Input 9999999 fails with requested fieldWidth of 6
	Returning a 'NaN' string.
Error in convert_integerToString: Input -999999 fails with requested fieldWidth of 6
	Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth > 15 not verified
	Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0 
	Returning a 'NaN' string.
Error in convert_integerToString: fieldWidth <= 0 
	Returning a 'NaN' string.
miscUtils Tests passed!

real	0m0.118s
user	0m0.012s
sys	0m0.010s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/miscUtilsTest passed (as expected)
=============================================

+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
+ /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest
vlmUtils Tests passed!

real	0m0.102s
user	0m0.012s
sys	0m0.009s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/vlmUtilsTest passed (as expected)
=============================================

+ rm -rf aimTest
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm
 Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch

 testingAIM/aimInitialize  instance = -1  unitSys = (null)!
 caps_queryAnalysis = 0  4 3 1
 testingAIM/aimInputs instance = -1  index = 1!
  in  1: testingAIMin   0
 testingAIM/aimInputs instance = -1  index = 2!
  in  2: table   0
 testingAIM/aimInputs instance = -1  index = 3!
  in  3: tessIn   0
 testingAIM/aimInputs instance = -1  index = 4!
  in  4: meshFile   0
 testingAIM/aimOutputs instance = -1  index = 1!
  out 1: testingAIMout   0
 testingAIM/aimOutputs instance = -1  index = 2!
  out 2: tessOut   0
 testingAIM/aimOutputs instance = -1  index = 3!
  out 3: meshFile   0


 testingAIM/aimInitialize  instance = 0  unitSys = m!
 testingAIM/aimInputs instance = 0  index = 1!
 testingAIM/aimInputs instance = 0  index = 2!
 testingAIM/aimInputs instance = 0  index = 3!
 testingAIM/aimInputs instance = 0  index = 4!
 testingAIM/aimOutputs instance = 0  index = 1!
 testingAIM/aimOutputs instance = 0  index = 2!
 testingAIM/aimOutputs instance = 0  index = 3!
 testingAIM/aimBackdoor instance = 0: Input String!
 Backdoor return string = aimBackdoor Output

 testingAIM/aimInitialize  instance = 1  unitSys = (null)!
 testingAIM/aimInputs instance = 1  index = 1!
 testingAIM/aimInputs instance = 1  index = 2!
 testingAIM/aimInputs instance = 1  index = 3!
 testingAIM/aimInputs instance = 1  index = 4!
 testingAIM/aimOutputs instance = 1  index = 1!
 testingAIM/aimOutputs instance = 1  index = 2!
 testingAIM/aimOutputs instance = 1  index = 3!

 Intent  = child
 APath   = /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/test/aimTest/Scratch/testingAIM1
 UnitSys = (null)
 Exec    = 1
 Fields  =  scalar (1 1)  vector (3 1)  scalar (1 0)  vector (3 0)
 Dirty   =  3

 Problem: # Dirty Analyses = 2!
 Bound:   # Dirty Analyses = 2!
 Analys0: # Dirty Analyses = 0!
 Analys1: # Dirty Analyses = 1!
 testingAIM/aimUpdateState instance = 0!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 0!
 testingAIM/aimPreAnalysis aim_getBounds = 0
   Analysis in Bound = Interface
     aim_newGeometry = 0!
   getDiscr = 0
   getDataSet = 0, rank = 1, method = 0
   0 scalars!
   meshRef = NULL
 testingAIM/aimExecute instance = 0!
 testingAIM/aimPostAnalysis instance = 0  restart = 0!
 testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
 After Execute on Parent

 Problem: # Dirty Analyses = 1!
 Bound:   # Dirty Analyses = 1!
 Analys0: # Dirty Analyses = 0!
 Analys1: # Dirty Analyses = 0!
 testingAIM/aimCalcOutput instance = 0  index = 2 tessOut 0!
 tessPtr = 0
 testingAIM/aimUpdateState instance = 1!
   tess is NULL!
 testingAIM/aimDiscr: tname = Interface, instance = 1!
 testingAIM/aimDiscr: Tessellation set!
 testingAIM/aimDiscr: Body 1/Face 3 matches Interface!
 testingAIM/aimDiscr: ntris = 1962!
 testingAIM/aimDiscr: npts = 1040!
 testingAIM/aimDiscr: tname = Interface, instance = 0!
 testingAIM/aimDiscr: Tessellation set!
 testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
 testingAIM/aimDiscr: ntris = 790!
 testingAIM/aimDiscr: npts = 442!
 testingAIM/aimTransfer name = scalar  instance = 0  npts = 442/1!
 CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
            Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 3.844036e-11
 testingAIM/aimPreAnalysis instance = 1!
 testingAIM/aimPreAnalysis aim_getBounds = 0
   Analysis in Bound = Interface
     aim_newGeometry = 0!
   getDiscr = 0
   getDataSet = -303, rank = 0, method = 0
   vectors not setup yet!
 testingAIM/aimExecute instance = 1!
 testingAIM/aimPostAnalysis instance = 1  restart = 0!

 Dirty    =  0

 Problem: # Dirty Analyses = 0!
 Bound:   # Dirty Analyses = 0!
 Analys0: # Dirty Analyses = 0!
 Analys1: # Dirty Analyses = 0!

 Body 1 has length units = cm
 Body 2 has length units = cm

 aimTest has type PROBLEM, subtype PARAMETRIC with 0 attributes
   last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
   hist: (null) -> Initial Phase
         aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
   2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds

   ParamName has type VALUE, subtype PARAMETER with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  2
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  2
     value = 0.000000 (null)
   Param has type VALUE, subtype PARAMETER with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  3
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  3
     value = 99 (null)

   num has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  6
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  6
     value = 8.000000 (null)
   x has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     value (8x1) = 7.300000 8.400000 10.400000 11.300000 12.300000 13.800000 14.400000 17.200000 (null)
   ymin has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     value (8x1) = -1.250000 -1.900000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 -2.100000 (null)
   zmin has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     value (8x1) = -0.825000 -0.812500 -0.800000 -0.775000 -0.750000 -0.700000 -0.690000 -0.100000 (null)
   zmax has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     value (8x1) = 0.825000 0.812500 0.800000 0.775000 0.750000 0.700000 0.690000 0.100000 (null)
   unused has type VALUE, subtype GEOMETRYIN with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  7
     hist: (null) -> Initial Phase
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  1
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  7
     linked to ParamName

   pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  16
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  16
     value = 34.641525 (null)
   cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  16
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  16
     value = 7.296560 (null)

   testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       value = 5.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       value (1x3) =
        1: Entry1 -> Value1
        2: Entry2 -> Value2
        3: Entry3 -> Value3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  8
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  9
 testingAIM/aimCalcOutput instance = 0  index = 1 testingAIMout 0!
 aim_getDiscr 0 on Interface = 0
 aim_getDataSet 0 on Interface = -329
       value = 12.340000 cm
       lazy: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:44  18
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
       hist: (null) -> Child Execute
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
       value (0x0) = NULL with len = 0 ego
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  9
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:44  18

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
       value = 42 (null)
   testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  28
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
     hist: (null) -> Child Execute
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  28
     4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
     1 Bodies, 1 Tessellations

     testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  10
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  10
       value = 6.000000 cm
     table has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  12
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  12
       value (1x3) =
        1: Entry1 -> newValue1
        2: Entry2 -> newValue2
        3: Entry3 -> newValue3
     tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  18
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  13
       hist: (null) -> Child Execute
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
       linked to tessOut
     meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  10
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  10
       value (0x0) = NULL with len = 0 writer

     testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  11
 testingAIM/aimCalcOutput instance = 1  index = 1 testingAIMout 0!
 aim_getDiscr 1 on Interface = 0
 aim_getDataSet 1 on Interface = -329
       value = 12.340000 cm
       lazy: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:44  28
     tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  11
 testingAIM/aimCalcOutput instance = 1  index = 2 tessOut 0!
 tessPtr = 7f98aba04800
       value = 7f98aba04800 ego
       lazy: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:44  28
     meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  11
 testingAIM/aimCalcOutput instance = 1  index = 3 meshFile 0!
       value (0x0) = NULL with len = 0 writer
       lazy: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:44  28

     Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  28
       hist: (null) -> Child Execute
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  28
       value = 42 (null)

   Interface has type BOUND, subtype NONE with 0 attributes
     last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
     hist: (null) -> Starting
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  14
     hist: (null) -> Child Execute
           aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
     2 Connecteds, 0 UnConnecteds

     testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
       hist: (null) -> Child Execute
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
       5 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         1040 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         1040 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  26
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  15
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:43  26
         1040 points, rank=1, units=(null)
     testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
       last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
       hist: (null) -> Starting
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
       hist: (null) -> Child Execute
             aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
       6 DataSets

       xyz has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         442 points, rank=3, units=cm
       xyzd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         0 points, rank=3, units=(null)
       param has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  23
         442 points, rank=2, units=(null)
       paramd has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         0 points, rank=2, units=(null)
       scalar has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  25
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Child Execute
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:20  25
         442 points, rank=1, units=(null)
       vector has type DATASET, subtype NONE with 0 attributes
         last: aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
         hist: (null) -> Starting
               aimTest macys-VM:66106 jenkins  2022/12/02  00:14:19  0
 testingAIM/aimTransfer name = vector  instance = 0  npts = 442/3!
         442 points, rank=3, units=(null)

    1: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
    8: 14.400000 14.400000 14.400000 14.400000 14.400000 14.381076 14.400000
   15: 14.400000 14.385654 14.400000 14.386399 14.400000 14.400000 14.400000
   22: 14.400000 14.400000 14.400000 14.383470 14.400000 14.400000 14.400000
   29: 14.400000 14.390663 14.400000 14.400000 14.400000 14.400000 14.400000
   36: 14.400000 14.400000 14.390526 14.400000 14.400000 14.400000 14.400000
   43: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   50: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   57: 14.400000 14.400000 14.400000 14.400000 14.377038 14.400000 14.377947
   64: 14.400000 14.378370 14.400000 14.380439 14.400000 14.400000 14.400000
   71: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
   78: 14.390431 14.400000 14.400000 14.400000 14.391064 14.400000 14.384912
   85: 14.400000 14.400000 14.400000 14.400000 14.400000 14.390113 14.400000
   92: 14.400000 14.400000 14.400000 14.400000 14.388870 14.400000 14.400000
   99: 14.400000 14.400000 14.386035 14.400000 14.384898 14.400000 14.400000
  106: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  113: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  120: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  127: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  134: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  141: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  148: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  155: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  162: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  169: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  176: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  183: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  190: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  197: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  204: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  211: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  218: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  225: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  232: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  239: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  246: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  253: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  260: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  267: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  274: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  281: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  288: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  295: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  302: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  309: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  316: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  323: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  330: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  337: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  344: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  351: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  358: 14.382997 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  365: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  372: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  379: 14.400000 14.400000 14.400000 14.356448 14.400000 14.400000 14.400000
  386: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  393: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  400: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  407: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  414: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  421: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  428: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  435: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  442: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  449: 14.400000 14.360432 14.400000 14.400000 14.400000 14.400000 14.400000
  456: 14.400000 14.400000 14.363710 14.400000 14.400000 14.400000 14.400000
  463: 14.400000 14.400000 14.364299 14.400000 14.400000 14.400000 14.400000
  470: 14.400000 14.400000 14.400000 14.363289 14.400000 14.400000 14.362208
  477: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  484: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  491: 14.400000 14.400000 14.400000 14.365678 14.400000 14.400000 14.400000
  498: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363289 14.400000
  505: 14.400000 14.400000 14.400000 14.361522 14.400000 14.368098 14.400000
  512: 14.400000 14.363976 14.400000 14.400000 14.370432 14.400000 14.400000
  519: 14.400000 14.400000 14.400000 14.400000 14.400000 14.363968 14.400000
  526: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  533: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  540: 14.400000 14.400000 14.363289 14.400000 14.400000 14.363979 14.366708
  547: 14.368597 14.400000 14.400000 14.400000 14.400000 14.367920 14.400000
  554: 14.372633 14.400000 14.400000 14.400000 14.400000 14.362154 14.400000
  561: 14.400000 14.400000 14.400000 14.400000 14.400000 14.366708 14.400000
  568: 14.369034 14.400000 14.369841 14.371226 14.400000 14.400000 14.400000
  575: 14.400000 14.400000 14.368408 14.367520 14.400000 14.368432 14.400000
  582: 14.400000 14.400000 14.400000 14.366087 14.400000 14.400000 14.369959
  589: 14.367920 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  596: 14.369369 14.368144 14.400000 14.400000 14.400000 14.400000 14.400000
  603: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  610: 14.367841 14.372775 14.400000 14.400000 14.400000 14.372125 14.378179
  617: 14.400000 14.400000 14.400000 14.400000 14.369095 14.400000 14.400000
  624: 14.400000 14.400000 14.400000 14.400000 14.400000 14.367920 14.371353
  631: 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000 14.400000
  638: 14.400000 14.400000 14.400000 14.400000 14.377272 14.376093 14.400000
  645: 14.372738 14.400000 14.400000 14.370290 14.400000 14.400000 14.400000
  652: 14.400000 14.365824 14.376750 14.400000 14.371580 14.368734 14.400000
  659: 14.373031 14.400000 14.371453 14.400000 14.376424 14.373411 14.375742
  666: 14.379766 14.400000 14.400000 14.372722 14.400000 14.400000 14.372350
  673: 14.400000 14.369868 14.400000 14.379928 14.400000 14.400000 14.400000
  680: 14.400000 14.400000 14.372894 14.375220 14.400000 14.400000 14.400000
  687: 14.400000 14.400000 14.400000 14.379491 14.373945 14.373477 14.373204
  694: 14.369160 14.400000 14.400000 14.371245 14.400000 14.370144 14.400000
  701: 14.400000 14.367593 14.400000 14.400000 14.400000 14.400000 14.400000
  708: 14.377553 14.400000 14.400000 14.372777 14.400000 14.400000 14.400000
  715: 14.400000 14.374692 14.400000 14.400000 14.400000 14.373031 14.375837
  722: 14.400000 14.400000 14.370074 14.400000 14.380072 14.400000 14.400000
  729: 14.400000 14.400000 14.375022 14.372158 14.400000 14.373856 14.380242
  736: 14.400000 14.377974 14.400000 14.400000 14.380573 14.400000 14.400000
  743: 14.400000 14.400000 14.400000 14.370484 14.372158 14.375910 14.400000
  750: 14.381582 14.375912 14.400000 14.400000 14.379288 14.400000 14.373737
  757: 14.400000 14.400000 14.400000 14.379729 14.382285 14.378584 14.400000
  764: 14.382311 14.400000 14.400000 14.374409 14.371245 14.379232 14.373945
  771: 14.400000 14.376341 14.400000 14.400000 14.377043 14.378486 14.374858
  778: 14.382054 14.400000 14.383869 14.381636 14.377184 14.400000 14.400000
  785: 14.400000 14.372636 14.400000 14.368456 14.383921 14.400000 14.400000
  792: 14.383458 14.400000 14.400000 14.400000 14.400000 14.400000 14.381953
  799: 14.400000 14.374858 14.373072 14.378348 14.379772 14.400000 14.378216
  806: 14.378852 14.400000 14.400000 14.400000 14.380161 14.400000 14.400000
  813: 14.384556 14.381516 14.400000 14.376255 14.400000 14.380120 14.400000
  820: 14.400000 14.380472 14.379996 14.400000 14.373072 14.400000 14.373126
  827: 14.379728 14.388089 14.378410 14.377743 14.383644 14.400000 14.400000
  834: 14.381170 14.377592 14.376925 14.384404 14.383167 14.400000 14.382056
  841: 14.400000 14.383692 14.400000 14.383013 14.384733 14.400000 14.400000
  848: 14.400000 14.380633 14.400000 14.400000 14.400000 14.373808 14.381358
  855: 14.400000 14.400000 14.383124 14.400000 14.400000 14.385360 14.376255
  862: 14.373590 14.400000 14.383049 14.386052 14.382506 14.381131 14.383698
  869: 14.384781 14.379968 14.383657 14.384709 14.377957 14.400000 14.380975
  876: 14.400000 14.375227 14.400000 14.379017 14.378731 14.378357 14.376010
  883: 14.373652 14.383370 14.383357 14.385444 14.385424 14.381819 14.384645
  890: 14.379402 14.389897 14.380433 14.400000 14.383857 14.385410 14.384756
  897: 14.379335 14.385835 14.400000 14.385091 14.374477 14.383079 14.383855
  904: 14.380149 14.374722 14.383296 14.381983 14.376090 14.383810 14.378363
  911: 14.387375 14.383245 14.378412 14.383393 14.382951 14.382465 14.382804
  918: 14.384507 14.385472 14.385336 14.385820 14.384140 14.385028 14.385702
  925: 14.383042 14.388214 14.388256 14.382050 14.381706 14.379795 14.381159
  932: 14.381897 14.378803 14.384372 14.381369 14.386079 14.387357 14.385924
  939: 14.382744 14.381612 14.381032 14.386745 14.385849 14.379042 14.385090
  946: 14.400000 14.381764 14.381240 14.379650 14.385693 14.385693 14.386153
  953: 14.384626 14.387791 14.385449 14.400000 14.385665 14.400000 14.379731
  960: 14.380272 14.385409 14.385781 14.381733 14.382438 14.385533 14.380583
  967: 14.386516 14.384573 14.400000 14.378382 14.384594 14.400000 14.386153
  974: 14.382680 14.389375 14.386802 14.381707 14.379398 14.380377 14.386666
  981: 14.387596 14.388630 14.387987 14.379180 14.386395 14.386595 14.400000
  988: 14.385128 14.382720 14.381637 14.387158 14.381496 14.389287 14.386767
  995: 14.382154 14.388300 14.384113 14.381877 14.390676 14.383198 14.387762
 1002: 14.386642 14.388993 14.383485 14.387635 14.390869 14.381952 14.382376
 1009: 14.381221 14.379752 14.400000 14.382249 14.378060 14.383886 14.382511
 1016: 14.387091 14.386270 14.384482 14.387626 14.381697 14.387252 14.400000
 1023: 14.378331 14.384910 14.381021 14.388566 14.400000 14.388325 14.387032
 1030: 14.378428 14.387252 14.379752 14.400000 14.384558 14.384911 14.381221
 1037: 14.378848 14.384694 14.382523 14.382981
 source getTriangles = 0, nGtris = 1962, nGsegs = 5886, Ds = 0 0
 destin getTriangles = 0, nGtris = 790, nGsegs = 2370, Ds = 0 0
 testingAIM/aimCleanup   instance = 0!
 testingAIM/aimCleanup   instance = 1!

real	0m26.327s
user	0m20.688s
sys	0m0.631s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/aim testingAIM.csm passed (as expected)
=============================================

+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm

 testingAIM/aimInitialize  instance = 0  unitSys = m!
 testingAIM/aimInputs instance = 0  index = 1!
 testingAIM/aimInputs instance = 0  index = 2!
 testingAIM/aimInputs instance = 0  index = 3!
 testingAIM/aimInputs instance = 0  index = 4!
 testingAIM/aimOutputs instance = 0  index = 1!
 testingAIM/aimOutputs instance = 0  index = 2!
 testingAIM/aimOutputs instance = 0  index = 3!

 testingAIM/aimInitialize  instance = 1  unitSys = (null)!
 testingAIM/aimInputs instance = 1  index = 1!
 testingAIM/aimInputs instance = 1  index = 2!
 testingAIM/aimInputs instance = 1  index = 3!
 testingAIM/aimInputs instance = 1  index = 4!
 testingAIM/aimOutputs instance = 1  index = 1!
 testingAIM/aimOutputs instance = 1  index = 2!
 testingAIM/aimOutputs instance = 1  index = 3!

 Intent  = child
 APath   = /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM1
 UnitSys = (null)
 Exec    = 2
 Fields  =  scalar (1 1)  vector (3 1)  scalar (1 0)  vector (3 0)
 Dirty   =  3

 testingAIM/aimUpdateState instance = 0!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 0!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   getDiscr = -303
   meshRef = NULL
 testingAIM/aimExecute instance = 0!
 testingAIM/aimPostAnalysis instance = 0  restart = 0!
 testingAIM/aimPostAnalysis: 0 -- 1 is Config Parameter
 testingAIM/aimCalcOutput instance = 0  index = 1 testingAIMout 0!
 aim_getDiscr 0 on Interface = -303
 testingAIM/aimCalcOutput instance = 0  index = 3 meshFile 0!
 testingAIM/aimUpdateState instance = 1!
   tess is NULL!
 testingAIM/aimPreAnalysis instance = 1!
 testingAIM/aimPreAnalysis aim_getBounds = 0
     aim_newGeometry = 0!
   mesh file = /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/CAPS/test/autoExecTest/Scratch/testingAIM0/meshFile
   symLink  = 0
   getDiscr = -303
 testingAIM/aimExecute instance = 1!
 testingAIM/aimPostAnalysis instance = 1  restart = 0!
 testingAIM/aimCalcOutput instance = 1  index = 1 testingAIMout 0!
 aim_getDiscr 1 on Interface = -303

 *** testingAIMout (child) = 12.340000  1 1 ***

 testingAIM/aimCleanup   instance = 0!
 testingAIM/aimCleanup   instance = 1!

real	0m0.884s
user	0m0.532s
sys	0m0.143s
+ set +x

=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64/ESP/DARWIN64/test/autoExec testingAIM.csm passed (as expected)
=============================================

++ set +x
[Execution node] check if [macys_VM] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.4/CAPS/unit/DARWIN64')
[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_RegCaps/7.4/CAPS/unit/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,CAPS/unit,DARWIN64,macys_VM)
[Static Analysis] Using reference build 'ESP_RegCaps/CASREV=7.4,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys_VM #469' 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_RegCaps/CASREV=7.4,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN64,buildnode=macys_VM #470'.
[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