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AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.200   seconds
Body 1 (of 2)
Number of nodes    = 4925
Number of elements = 9846
Number of triangle elements      = 9846
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 8
Number of elements = 12
Number of triangle elements      = 12
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4933
Total number of elements = 9858
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

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    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

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     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 13.1976
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.309
AFLR4    : Abs Min Surf Spacing        = 0.032994
AFLR4    : Min Surf Spacing            = 0.065988
AFLR4    : Max Surf Spacing            = 1.31976
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
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=      9858
AFLR43   : Nodes             =      4933
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 22.6.0 x86_64
AFLR3    : Compile Date   11/01/23 @ 12:19PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      4933         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                      FarField
UG3      :         12                      FarField
UG3      :         13                      FarField
UG3      :         14                      FarField
UG3      :         15                      FarField
UG3      :         16                      FarField
 
AFLR3    : CPU Time          =     0.011   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      4933         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =       988      7142
AFLR3 IG : Nodes, Elements   =      1976     14311
AFLR3 IG : Nodes, Elements   =      2964     22901
AFLR3 IG : Nodes, Elements   =      3952     31940
AFLR3 IG : Nodes, Elements   =      4940     40111
AFLR3 IG : Nodes, Elements   =      4940     40004
AFLR3 IG : Nodes, Elements   =      4940     40007
AFLR3 IG : Nodes, Elements   =      4940     39931
AFLR3 IG : Nodes, Elements   =      4933     25885
AFLR3 IG : Nodes, Elements   =      4933     26051
AFLR3 IG : Nodes, Elements   =      4933     14490
AFLR3 IG : Nodes, Elements   =      4933     13234
 
AFLR3    : CPU Time          =     0.145   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      4933     13234
AFLR3 GG : Nodes, Elements   =      4987     13396
AFLR3 GG : Nodes, Elements   =      4987     13472
AFLR3 GG : Nodes, Elements   =      4987     13267
AFLR3 GG : Nodes, Elements   =      5017     13357
AFLR3 GG : Nodes, Elements   =      5017     13615
AFLR3 GG : Nodes, Elements   =      5017     13543
AFLR3 GG : Nodes, Elements   =      5078     13727
AFLR3 GG : Nodes, Elements   =      5078     13891
AFLR3 GG : Nodes, Elements   =      5078     13446
AFLR3 GG : Nodes, Elements   =      5165     13707
AFLR3 GG : Nodes, Elements   =      5165     14180
AFLR3 GG : Nodes, Elements   =      5165     13827
AFLR3 GG : Nodes, Elements   =      5224     14004
AFLR3 GG : Nodes, Elements   =      5224     14359
AFLR3 GG : Nodes, Elements   =      5224     14077
AFLR3 GG : Nodes, Elements   =      5268     14209
AFLR3 GG : Nodes, Elements   =      5268     14458
AFLR3 GG : Nodes, Elements   =      5268     14303
AFLR3 GG : Nodes, Elements   =      5300     14399
AFLR3 GG : Nodes, Elements   =      5300     14636
AFLR3 GG : Nodes, Elements   =      5300     14496
AFLR3 GG : Nodes, Elements   =      5321     14559
AFLR3 GG : Nodes, Elements   =      5321     14707
AFLR3 GG : Nodes, Elements   =      5321     14603
AFLR3 GG : Nodes, Elements   =      5336     14648
AFLR3 GG : Nodes, Elements   =      5336     14741
AFLR3 GG : Nodes, Elements   =      5336     14666
AFLR3 GG : Nodes, Elements   =      5344     14690
AFLR3 GG : Nodes, Elements   =      5344     14728
AFLR3 GG : Nodes, Elements   =      5344     14710
AFLR3 GG : Nodes, Elements   =      5348     14722
AFLR3 GG : Nodes, Elements   =      5348     14753
AFLR3 GG : Nodes, Elements   =      5348     14733
AFLR3 GG : Nodes, Elements   =      5350     14739
AFLR3 GG : Nodes, Elements   =      5350     14746
AFLR3 GG : Nodes, Elements   =      5350     14743
AFLR3 GG : Nodes, Elements   =      5353     14752
AFLR3 GG : Nodes, Elements   =      5353     14766
AFLR3 GG : Nodes, Elements   =      5353     14760
 
AFLR3    : CPU Time          =     0.081   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =      5353     14760
AFLR3 QI : Nodes, Elements   =      5305     14479
AFLR3 QI : Nodes, Elements   =      5281     14338
AFLR3 QI : Nodes, Elements   =      5274     14298
AFLR3 QI : Nodes, Elements   =      5273     14292
AFLR3 QI : Nodes, Elements   =      5273     19714
AFLR3 QI : Nodes, Elements   =      5273     15107
AFLR3 QI : Nodes, Elements   =      5273     13825
AFLR3 QI : Nodes, Elements   =      5273     19727
AFLR3 QI : Nodes, Elements   =      5273     15071
AFLR3 QI : Nodes, Elements   =      5273     13896
AFLR3 QI : Nodes, Elements   =      5273     19727
AFLR3 QI : Nodes, Elements   =      5273     15059
AFLR3 QI : Nodes, Elements   =      5273     13749
AFLR3 QI : Nodes, Elements   =      5273     19724
AFLR3 QI : Nodes, Elements   =      5273     15101
AFLR3 QI : Nodes, Elements   =      5273     13821
AFLR3 QI : Nodes, Elements   =      5273     19722
AFLR3 QI : Nodes, Elements   =      5273     15081
AFLR3 QI : Nodes, Elements   =      5273     13905
AFLR3 QI : Nodes, Elements   =      5273     13725
AFLR3 QI : Nodes, Elements   =      5317     13899
AFLR3 QI : Nodes, Elements   =      5317     21044
AFLR3 QI : Nodes, Elements   =      5317     14814
AFLR3 QI : Nodes, Elements   =      5317     14269
AFLR3 QI : Nodes, Elements   =      5317     17679
AFLR3 QI : Nodes, Elements   =      5317     14301
AFLR3 QI : Nodes, Elements   =      5317     13830
 
AFLR3    : CPU Time          =     0.321   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =      5317     13830
 
AFLR3    : CPU Time          =     0.004   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Ang      =  0.006596     179.7
UG3      : Average Angle     =      73.4
UG3      : No. Angle>160.0   =      1922
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =     13830
UG3      : Min Vol           =  0.000293
UG3      : Average Vol       =  4.31e+06
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Q        =  1.25e-05         1
UG3      : Average Q         =     0.106
UG3      : No. Q<       0.1  =     10496
UG3      : No. Q<      0.01  =      8943

OVERALL  : CPU Time          =     0.571   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Ang      =  0.006596     179.7
UG3      : Average Angle     =      73.4
UG3      : No. Angle>160.0   =      1922
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =     13830
UG3      : Min Vol           =  0.000293
UG3      : Average Vol       =  4.31e+06
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Q        =    0.0034         1
UG3      : Average Q         =     0.186
UG3      : No. Q<       0.1  =      8713
UG3      : No. Q<      0.01  =        59

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 18

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 10

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
	Number of nodes          = 5317
	Number of elements       = 23688
	Number of triangles      = 9858
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 13830
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_inviscidWing.dat.
Surface file name: surface_flow_inviscidWing.
Volume file name: flow_inviscidWing.
Restart file name: restart_flow_inviscidWing.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
5317 grid points.
13830 volume elements.
2 surface markers.
9846 boundary elements in index 0 (Marker = BC_1).
12 boundary elements in index 1 (Marker = BC_2).
13830 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 17.3483. Mean K: 1.87862. Standard deviation K: 2.72111.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.51936|        87.7801|
|     CV Face Area Aspect Ratio|        1.28339|    2.80217e+07|
|           CV Sub-Volume Ratio|        1.04782|    3.92559e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      5317|    1/1.00|        10|
|         1|      1307|    1/4.07|   9.39639|
|         2|       226|    1/5.78|   7.85229|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8234.67 m^2.
Area projection in the x-plane = 668.083 m^2, y-plane = 415.155 m^2, z-plane = 3916.84 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 50 m, y-direction = -97.6729 m, z-direction = -8.4717 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        221265|             1|   m^2/s^2|        221265|
|            Velocity-X|       170.123|             1|       m/s|       170.123|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|        2.9695|             1|       m/s|        2.9695|
|    Velocity Magnitude|       170.149|             1|       m/s|       170.149|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.6138e-01|    2.023460|    4.397129|    3.783010|    7.506305|    1.863179|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.6048e-01|    4.298015|    6.714837|    6.542729|    9.789782|    2.132951|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.5844e-01|    4.727771|    7.148676|    6.733970|   10.230267|    2.515644|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.5663e-01|    4.773027|    7.165669|    7.046496|   10.260358|    2.852228|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.5788e-01|    5.045623|    7.601076|    7.458299|   10.551039|    3.202407|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.6055e-01|    5.480149|    8.071079|    7.881620|   11.000946|    3.150787|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.5884e-01|    5.923301|    8.498020|    8.321209|   11.442224|    3.961853|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.5878e-01|    6.372453|    8.936643|    8.772539|   11.885227|    2.522149|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.5925e-01|    6.808587|    9.391142|    9.225137|   12.333941|   17.477646|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.5951e-01|    7.352488|    9.860621|    9.802983|   12.785819|   61.507480|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.35249|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_inviscidWing.dat      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|CSV file                           |surface_flow_inviscidWing.csv      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview                           |flow_inviscidWing.vtu              |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview surface                   |surface_flow_inviscidWing.vtu      |

Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


==> Total Forces and Moments
--> Cl =  1.490125 Cd =  0.024227
--> Cmx =  -0.102917 Cmy =  -0.21191 Cmz =  -0.012195
--> Cx =  -0.001783 Cy =  -0.054054 Cz =  1.490321

real	0m8.994s
user	0m4.612s
sys	0m2.559s
+ status=0
+ set +x

=================================================
data/session08/2_su2_InviscidWing.py passed (as expected)
=================================================


=================================================
1_astros_ModalCantilever.py test;
+ python 1_astros_ModalCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log

==> Loading geometry from file "../ESP/transport.csm"...

==> Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
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 = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
	Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
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 - EigenAnalysis
	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....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==> Running mASTROS...

==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10

--> Eigen-frequencies:
    1 : 0.00145606
    2 : 0.0014575
    3 : 0.00332859
    4 : 0.00333096
    5 : 0.00445176
    6 : 0.00445507
    7 : 0.00894917
    8 : 0.0089521
    9 : 0.0110353
    10: 0.0110413

real	1m11.122s
user	1m6.837s
sys	0m37.037s
+ status=0
+ set +x

=================================================
data/session09/1_astros_ModalCantilever.py passed (as expected)
=================================================


=================================================
2_astros_ModalSupport.py test;
+ python 2_astros_ModalSupport.py
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log

==> Loading geometry from file "../ESP/transport.csm"...

==> Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
	Name = ribSupport, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 831
Number of elements = 962
Number of triangle elements      = 0
Number of quadrilateral elements = 962
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 832
Total number of elements = 962
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 2
	Name = leftPointLoad, index = 1
	Name = ritePointLoad, index = 2
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = ribRoot, 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 = 6
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
	Name = ribSupport, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 831
	Number of elements = 962
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 962
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 832
	Combined Number of elements = 963
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 962
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - leftWingSkin
	Property name - ribSupport
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribRootPoint
	No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement"
	No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name
	Done getting FEA constraints

Getting FEA supports.......
	Number of supports - 1
	Support name - ribRootPoint
	No "groupName" specified for Support tuple ribRootPoint, going to use support name
	Done getting FEA supports

Getting FEA connections.......
	Number of connection tuples - 1
	Connection name - ribRoot
	No "groupName" specified for Connection tuple ribRoot!
	Looking for automatic connections from the use of capsConnectLink for ribRoot
	9 automatic connections were made for capsConnect ribRoot (node id 832)
	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 - EigenAnalysis
	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 connection cards - appending mesh file

Writing Astros instruction file....
	Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
	Writing analysis cards
	Writing constraint cards--all constraints for each subcase
	Writing support cards
	Writing material cards
	Writing property cards
	Writing coordinate system cards

==> Running mASTROS...

==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
	Number of Eigen-Values = 10
	Loading Eigen-Value = 1
	Loading Eigen-Value = 2
	Loading Eigen-Value = 3
	Loading Eigen-Value = 4
	Loading Eigen-Value = 5
	Loading Eigen-Value = 6
	Loading Eigen-Value = 7
	Loading Eigen-Value = 8
	Loading Eigen-Value = 9
	Loading Eigen-Value = 10

--> Eigen-frequencies:
    1 : 1.93141e-08
    2 : 0.0014201
    3 : 0.00174471
    4 : 0.00323704
    5 : 0.00324327
    6 : 0.00432932
    7 : 0.00512433
    8 : 0.00873482
    9 : 0.0100619
    10: 0.0107025

real	4m4.568s
user	3m30.957s
sys	1m33.749s
+ status=0
+ set +x

=================================================
data/session09/2_astros_ModalSupport.py passed (as expected)
=================================================


=================================================
3_astros_StaticCantilever.py test;
+ python 3_astros_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log

==> Loading geometry from file "../ESP/transport.csm"...

==> Running mASTROS pre-analysis...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
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 = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 2
	Load name - leftPointLoad
	No "groupName" specified for Load tuple leftPointLoad, going to use load name
	Load name - ritePointLoad
	No "groupName" specified for Load tuple ritePointLoad, going to use load name
	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
	Writing coordinate system cards

==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

==> Running mASTROS post-analysis...

--> Maximum displacements:
--> Tmax 238433.3403112283
--> T1max 16861.9
--> T2max 16414.9
--> T3max 237286.0

real	0m27.049s
user	0m40.296s
sys	0m18.971s
+ status=0
+ set +x

=================================================
data/session09/3_astros_StaticCantilever.py passed (as expected)
=================================================


=================================================
4_astros_Composite.py test;
+ python 4_astros_Composite.py
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log

==> Loading geometry from file "../ESP/transport.csm"...

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle


==> Running mASTROS pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
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 = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Aluminum
	No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
	Material name - Graphite_epoxy
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

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

Getting FEA loads.......
	Number of loads - 2
	Load name - leftPointLoad
	No "groupName" specified for Load tuple leftPointLoad, going to use load name
	Load name - ritePointLoad
	No "groupName" specified for Load tuple ritePointLoad, going to use load name
	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
	Writing coordinate system cards

==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

==> Running mASTROS post-analysis...

--> Maximum displacements:
--> Tmax 52594.60117638786
--> T1max 4359.68
--> T2max 3216.5
--> T3max 52322.2

real	0m27.802s
user	0m41.478s
sys	0m21.666s
+ status=0
+ set +x

=================================================
data/session09/4_astros_Composite.py passed (as expected)
=================================================

Traceback (most recent call last):
  File "<string>", line 1, in <module>
ModuleNotFoundError: No module named 'tacs'

=================================================
2_aeroelastic_Iterative_SU2_Astros.py test;
+ python 2_aeroelastic_Iterative_SU2_Astros.py
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log

MESSAGE:: Building wingOml


MESSAGE:: Building wingWaffle


==> Running SU2 pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Mesh sizing name - leftWing
	Mesh sizing name - riteWing
	Done getting mesh sizing parameters
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

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    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

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     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 21.7051
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 2651.51
AFLR4    : Abs Min Surf Spacing        = 0.0542627
AFLR4    : Min Surf Spacing            = 0.108525
AFLR4    : Max Surf Spacing            = 2.17051
AFLR4    : Global Scale Factor         = 5

AFLR4    : Geometry Definition Information

AFLR4    : Definition              Definition   Composite             Grid BC
AFLR4    :         ID                    Type          ID                Type
AFLR4    :          0     glue-only composite           -                   -
AFLR4    :          1            CAD geometry           0            STD w/BL
AFLR4    :          2            CAD geometry           0            STD w/BL
AFLR4    :          3            CAD geometry           0            STD w/BL
AFLR4    :          4            CAD geometry           0            STD w/BL
AFLR4    :          5            CAD geometry           0            STD w/BL
AFLR4    :          6            CAD geometry           0            STD w/BL
AFLR4    :          7            CAD geometry           0            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            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Trias,Quads=      1107      2082         0
AFLR4    : Nodes, Trias,Quads=       685      1238         0

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Trias,Quads=      1473      2759         0
AFLR4    : Nodes, Trias,Quads=       721      1255         0

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Trias,Quads=      1116      2100         0
AFLR4    : Nodes, Trias,Quads=       671      1210         0

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Trias,Quads=      1458      2729         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Trias,Quads=      1108      2084         0
AFLR4    : Nodes, Trias,Quads=       683      1234         0

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Trias,Quads=      1488      2789         0
AFLR4    : Nodes, Trias,Quads=       714      1241         0

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Trias,Quads=      1112      2092         0
AFLR4    : Nodes, Trias,Quads=       653      1174         0

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Trias,Quads=      1456      2725         0
AFLR4    : Nodes, Trias,Quads=       708      1229         0

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Trias,Quads=        20        24         0
AFLR4    : Nodes, Trias,Quads=        14        12         0

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Trias,Quads=         5         4         0
AFLR4    : Nodes, Trias,Quads=         4         2         0

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes,Faces,BEdges=      4933      9858      1312

AFLR4    : Auto Mode Turned OFF

OVERALL  : CPU Time          =     0.151   seconds
Body 1 (of 2)
Number of nodes    = 4925
Number of elements = 9846
Number of triangle elements      = 9846
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 8
Number of elements = 12
Number of triangle elements      = 12
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4933
Total number of elements = 9858
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = leftWing, index = 1
	Name = riteWing, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Farfield, index = 2
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.17.15
AFLR2    : Version Date   04/23/24 @ 12:51AM
AFLR2    : Compile OS     Darwin 23.4.0 x86_64
AFLR2    : Compile Date   04/23/24 @ 11:49AM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 11.5.14
AFLR4    : Version Date   04/18/24 @ 12:45PM
AFLR4    : Compile OS     Darwin 23.4.0 x86_64
AFLR4    : Compile Date   04/23/24 @ 11:49AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : EGADS CAD Geometry Setup

EGADS    : Model has 2 Active Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 Shells
EGADS    : Body 0 has 10 Faces
EGADS    : Body 0 has 18 Edges
EGADS    : Body 0 has 10 Loops
EGADS    : Body 0 has 10 Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 Shells
EGADS    : Body 1 has 6 Faces
EGADS    : Body 1 has 12 Edges
EGADS    : Body 1 has 6 Loops
EGADS    : Body 1 has 8 Nodes

EGADS    : Check Grid BCs

EGADS    : Grid BCs are OK

EGADS    : Face Neighbor-Faces Information

EGADS    : QC  = Face Quad Combination Flag
EGADS    : IER = Face Isolated Edge Refinement Flag
EGADS    : ER  = Face Edge Refinement Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.
EGADS    : SF  = Face Scale Factor
EGADS    :       Not applicable for Faces with a FarField Grid BC.

EGADS    :   Face          Body    QC   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     0     1        1        1   2 3 6
EGADS    :      2     Yes     0     0     1        1        1   1 4 5
EGADS    :      3     Yes     0     0     1        1        1   1 4 8
EGADS    :      4     Yes     0     0     1        1        1   2 3 5
EGADS    :      5     Yes     0     0     1        1        1   2 4
EGADS    :      6     Yes     0     0     1        1        1   1 7 8
EGADS    :      7     Yes     0     0     1        1        1   6 9 10
EGADS    :      8     Yes     0     0     1        1        1   3 6 9
EGADS    :      9     Yes     0     0     1        1        1   7 8 10
EGADS    :     10     Yes     0     0     1        1        1   7 9
EGADS    :     11     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     12     Yes     1     0     1       NA       NA   13 14 15 16
EGADS    :     13     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     14     Yes     1     0     1       NA       NA   11 12 15 16
EGADS    :     15     Yes     1     0     1       NA       NA   11 12 13 14
EGADS    :     16     Yes     1     0     1       NA       NA   11 12 13 14

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   -1 2 3 -4
EGADS    :      2   -5 4 6 -7
EGADS    :      3   -3 8 1 -9
EGADS    :      4   -6 9 5 -10
EGADS    :      5   7 10
EGADS    :      6   11 13 -12 -2
EGADS    :      7   14 16 -15 -13
EGADS    :      8   12 17 -11 -8
EGADS    :      9   15 18 -14 -17
EGADS    :     10   -16 -18
EGADS    :     11   19 20 -21 -22
EGADS    :     12   -23 26 25 -24
EGADS    :     13   27 23 -28 -19
EGADS    :     14   -29 21 30 -25
EGADS    :     15   22 29 -26 -27
EGADS    :     16   -20 28 24 -30

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    :     15   15
EGADS    :     16   16

EGADS    : Loop Edges Information

EGADS    :   Loop  Active   Edges
EGADS    :      1     Yes   -1 2 3 -4
EGADS    :      2     Yes   -5 4 6 -7
EGADS    :      3     Yes   -3 8 1 -9
EGADS    :      4     Yes   -6 9 5 -10
EGADS    :      5     Yes   7 10
EGADS    :      6     Yes   11 13 -12 -2
EGADS    :      7     Yes   14 16 -15 -13
EGADS    :      8     Yes   12 17 -11 -8
EGADS    :      9     Yes   15 18 -14 -17
EGADS    :     10     Yes   -16 -18
EGADS    :     11     Yes   19 20 -21 -22
EGADS    :     12     Yes   -23 26 25 -24
EGADS    :     13     Yes   27 23 -28 -19
EGADS    :     14     Yes   -29 21 30 -25
EGADS    :     15     Yes   22 29 -26 -27
EGADS    :     16     Yes   -20 28 24 -30

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     2        1   1 3
EGADS    :      2     0     Yes     1     3        1   1 6
EGADS    :      3     0     Yes     3     4        1   1 3
EGADS    :      4     0     Yes     2     4        1   1 2
EGADS    :      5     0     Yes     2     5        1   2 4
EGADS    :      6     0     Yes     4     6        1   2 4
EGADS    :      7     0     Yes     5     6        1   2 5
EGADS    :      8     0     Yes     3     1        1   3 8
EGADS    :      9     0     Yes     4     2        1   3 4
EGADS    :     10     0     Yes     6     5        1   4 5
EGADS    :     11     0     Yes     1     7        1   6 8
EGADS    :     12     0     Yes     3     8        1   6 8
EGADS    :     13     0     Yes     7     8        1   6 7
EGADS    :     14     0     Yes     7     9        1   7 9
EGADS    :     15     0     Yes     8    10        1   7 9
EGADS    :     16     0     Yes     9    10        1   7 10
EGADS    :     17     0     Yes     8     7        1   8 9
EGADS    :     18     0     Yes    10     9        1   9 10
EGADS    :     19     1     Yes    12    11       NA   11 13
EGADS    :     20     1     Yes    11    13       NA   11 16
EGADS    :     21     1     Yes    14    13       NA   11 14
EGADS    :     22     1     Yes    12    14       NA   11 15
EGADS    :     23     1     Yes    16    15       NA   12 13
EGADS    :     24     1     Yes    15    17       NA   12 16
EGADS    :     25     1     Yes    18    17       NA   12 14
EGADS    :     26     1     Yes    16    18       NA   12 15
EGADS    :     27     1     Yes    12    16       NA   13 15
EGADS    :     28     1     Yes    11    15       NA   13 16
EGADS    :     29     1     Yes    14    18       NA   14 15
EGADS    :     30     1     Yes    13    17       NA   14 16

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       97.2007855                0                0
EGADS    :      2     Yes       97.9335611                0                0
EGADS    :      3     Yes               50                0                0
EGADS    :      4     Yes       75.3047874                0                0
EGADS    :      5     Yes       123.552357                0        4.7180639
EGADS    :      6     Yes       118.391317                0       3.99272703
EGADS    :      7     Yes       97.9335611       36.1389817                0
EGADS    :      8     Yes       75.3047874       36.1389817                0
EGADS    :      9     Yes       123.552357       97.6729236        4.7180639
EGADS    :     10     Yes       118.391317       97.6729236       3.99272703
EGADS    :     11     Yes                0                0       1951.57774
EGADS    :     12     Yes                0                0                0
EGADS    :     13     Yes                0       1953.45847       1951.57774
EGADS    :     14     Yes                0       1953.45847                0
EGADS    :     15     Yes       2040.21562                0       1951.57774
EGADS    :     16     Yes       2040.21562                0                0
EGADS    :     17     Yes       2040.21562       1953.45847       1951.57774
EGADS    :     18     Yes       2040.21562       1953.45847                0

EGADS    : Face and Edge Match Information

EGADS    : No Face Matches Found

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 3906.92
AFLR4    : Min Bounding Box Length     = 3906.92
AFLR4    : Max Ref Bounding Box Length = 195.346
AFLR4    : Min Ref Bounding Box Length = 13.1976
AFLR4    : Reference Length            = 13.1976
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 428.309
AFLR4    : Abs Min Surf Spacing        = 0.032994
AFLR4    : Min Surf Spacing            = 0.065988
AFLR4    : Max Surf Spacing            = 1.31976
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
AFLR4    :          2            CAD geometry           0                 STD
AFLR4    :          3            CAD geometry           0                 STD
AFLR4    :          4            CAD geometry           0                 STD
AFLR4    :          5            CAD geometry           0                 STD
AFLR4    :          6            CAD geometry           0                 STD
AFLR4    :          7            CAD geometry           0                 STD
AFLR4    :          8            CAD geometry           0                 STD
AFLR4    :          9            CAD geometry           0                 STD
AFLR4    :         10            CAD geometry           0                 STD
AFLR4    :         11            CAD geometry           0            FARFIELD
AFLR4    :         12            CAD geometry           0            FARFIELD
AFLR4    :         13            CAD geometry           0            FARFIELD
AFLR4    :         14            CAD geometry           0            FARFIELD
AFLR4    :         15            CAD geometry           0            FARFIELD
AFLR4    :         16            CAD geometry           0            FARFIELD

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
 
AFLR43   : INPUT SURFACE MESH FROM TESS
 
AFLR43   : Quad Surface Faces=         0
AFLR43   : Tria Surface Faces=      9858
AFLR43   : Nodes             =      4933
 
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.32.50
AFLR3    : Version Date   10/31/23 @ 06:31PM
AFLR3    : Compile OS     Darwin 22.6.0 x86_64
AFLR3    : Compile Date   11/01/23 @ 12:19PM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      4933         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                         Solid
UG3      :          2                         Solid
UG3      :          3                         Solid
UG3      :          4                         Solid
UG3      :          5                         Solid
UG3      :          6                         Solid
UG3      :          7                         Solid
UG3      :          8                         Solid
UG3      :          9                         Solid
UG3      :         10                         Solid
UG3      :         11                      FarField
UG3      :         12                      FarField
UG3      :         13                      FarField
UG3      :         14                      FarField
UG3      :         15                      FarField
UG3      :         16                      FarField
 
AFLR3    : CPU Time          =     0.010   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      4933         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =       988      7142
AFLR3 IG : Nodes, Elements   =      1976     14311
AFLR3 IG : Nodes, Elements   =      2964     22901
AFLR3 IG : Nodes, Elements   =      3952     31940
AFLR3 IG : Nodes, Elements   =      4940     40111
AFLR3 IG : Nodes, Elements   =      4940     40004
AFLR3 IG : Nodes, Elements   =      4940     40007
AFLR3 IG : Nodes, Elements   =      4940     39931
AFLR3 IG : Nodes, Elements   =      4933     25885
AFLR3 IG : Nodes, Elements   =      4933     26051
AFLR3 IG : Nodes, Elements   =      4933     14490
AFLR3 IG : Nodes, Elements   =      4933     13234
 
AFLR3    : CPU Time          =     0.124   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      4933     13234
AFLR3 GG : Nodes, Elements   =      4987     13396
AFLR3 GG : Nodes, Elements   =      4987     13472
AFLR3 GG : Nodes, Elements   =      4987     13267
AFLR3 GG : Nodes, Elements   =      5017     13357
AFLR3 GG : Nodes, Elements   =      5017     13615
AFLR3 GG : Nodes, Elements   =      5017     13543
AFLR3 GG : Nodes, Elements   =      5078     13727
AFLR3 GG : Nodes, Elements   =      5078     13891
AFLR3 GG : Nodes, Elements   =      5078     13446
AFLR3 GG : Nodes, Elements   =      5165     13707
AFLR3 GG : Nodes, Elements   =      5165     14180
AFLR3 GG : Nodes, Elements   =      5165     13827
AFLR3 GG : Nodes, Elements   =      5224     14004
AFLR3 GG : Nodes, Elements   =      5224     14359
AFLR3 GG : Nodes, Elements   =      5224     14077
AFLR3 GG : Nodes, Elements   =      5268     14209
AFLR3 GG : Nodes, Elements   =      5268     14458
AFLR3 GG : Nodes, Elements   =      5268     14303
AFLR3 GG : Nodes, Elements   =      5300     14399
AFLR3 GG : Nodes, Elements   =      5300     14636
AFLR3 GG : Nodes, Elements   =      5300     14496
AFLR3 GG : Nodes, Elements   =      5321     14559
AFLR3 GG : Nodes, Elements   =      5321     14707
AFLR3 GG : Nodes, Elements   =      5321     14603
AFLR3 GG : Nodes, Elements   =      5336     14648
AFLR3 GG : Nodes, Elements   =      5336     14741
AFLR3 GG : Nodes, Elements   =      5336     14666
AFLR3 GG : Nodes, Elements   =      5344     14690
AFLR3 GG : Nodes, Elements   =      5344     14728
AFLR3 GG : Nodes, Elements   =      5344     14710
AFLR3 GG : Nodes, Elements   =      5348     14722
AFLR3 GG : Nodes, Elements   =      5348     14753
AFLR3 GG : Nodes, Elements   =      5348     14733
AFLR3 GG : Nodes, Elements   =      5350     14739
AFLR3 GG : Nodes, Elements   =      5350     14746
AFLR3 GG : Nodes, Elements   =      5350     14743
AFLR3 GG : Nodes, Elements   =      5353     14752
AFLR3 GG : Nodes, Elements   =      5353     14766
AFLR3 GG : Nodes, Elements   =      5353     14760
 
AFLR3    : CPU Time          =     0.071   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =      5353     14760
AFLR3 QI : Nodes, Elements   =      5305     14479
AFLR3 QI : Nodes, Elements   =      5281     14338
AFLR3 QI : Nodes, Elements   =      5274     14298
AFLR3 QI : Nodes, Elements   =      5273     14292
AFLR3 QI : Nodes, Elements   =      5273     19714
AFLR3 QI : Nodes, Elements   =      5273     15107
AFLR3 QI : Nodes, Elements   =      5273     13825
AFLR3 QI : Nodes, Elements   =      5273     19727
AFLR3 QI : Nodes, Elements   =      5273     15071
AFLR3 QI : Nodes, Elements   =      5273     13896
AFLR3 QI : Nodes, Elements   =      5273     19727
AFLR3 QI : Nodes, Elements   =      5273     15059
AFLR3 QI : Nodes, Elements   =      5273     13749
AFLR3 QI : Nodes, Elements   =      5273     19724
AFLR3 QI : Nodes, Elements   =      5273     15101
AFLR3 QI : Nodes, Elements   =      5273     13821
AFLR3 QI : Nodes, Elements   =      5273     19722
AFLR3 QI : Nodes, Elements   =      5273     15081
AFLR3 QI : Nodes, Elements   =      5273     13905
AFLR3 QI : Nodes, Elements   =      5273     13725
AFLR3 QI : Nodes, Elements   =      5317     13899
AFLR3 QI : Nodes, Elements   =      5317     21044
AFLR3 QI : Nodes, Elements   =      5317     14814
AFLR3 QI : Nodes, Elements   =      5317     14269
AFLR3 QI : Nodes, Elements   =      5317     17679
AFLR3 QI : Nodes, Elements   =      5317     14301
AFLR3 QI : Nodes, Elements   =      5317     13830
 
AFLR3    : CPU Time          =     0.280   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =      5317     13830
 
AFLR3    : CPU Time          =     0.005   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Ang      =  0.006596     179.7
UG3      : Average Angle     =      73.4
UG3      : No. Angle>160.0   =      1922
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =     13830
UG3      : Min Vol           =  0.000293
UG3      : Average Vol       =  4.31e+06
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Q        =  1.25e-05         1
UG3      : Average Q         =     0.106
UG3      : No. Q<       0.1  =     10496
UG3      : No. Q<      0.01  =      8943

OVERALL  : CPU Time          =     0.502   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Ang      =  0.006596     179.7
UG3      : Average Angle     =      73.4
UG3      : No. Angle>160.0   =      1922
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  5.96e+10

UG3      : No. Tet Elems     =     13830
UG3      : Min Vol           =  0.000293
UG3      : Average Vol       =  4.31e+06
UG3      : Total-Tet-Vol     =  5.96e+10
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1
UG3      : Note that L includes scaling for BL-aspect=ratio

UG3      : No. Tet Elems     =     13830
UG3      : Min, Max Q        =    0.0034         1
UG3      : Average Q         =     0.186
UG3      : No. Q<       0.1  =      8713
UG3      : No. Q<      0.01  =        59

UG3      : CPU Time          =     0.000   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
EGADS    : OpenCASCADE Version 7.8.0
EGADS    : ---------------------------------------

EGADS    : CREATE EGADS TESS FROM AFLR3 DATA

EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS    : CREATING TESSELLATION FOR BODY 0 EDGE 18

EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS    : CREATING TESSELLATION FOR BODY 0 FACE 10

EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS    : CREATING TESSELLATION FOR BODY 1 EDGE 30

EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS    : CREATING TESSELLATION FOR BODY 1 FACE 16

EGADS    : EGADS TESS CREATED

EGADS    : CHECK TESS FACE NODE MAP

EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS    : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS    : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
	Number of nodes          = 5317
	Number of elements       = 23688
	Number of triangles      = 9858
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 13830
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing
	Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

==> Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
5317 grid points.
13830 volume elements.
2 surface markers.
9846 boundary elements in index 0 (Marker = BC_1).
12 boundary elements in index 1 (Marker = BC_2).
13830 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 17.3483. Mean K: 1.87862. Standard deviation K: 2.72111.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.51936|        87.7801|
|     CV Face Area Aspect Ratio|        1.28339|    2.80217e+07|
|           CV Sub-Volume Ratio|        1.04782|    3.92559e+08|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      5317|    1/1.00|        10|
|         1|      1307|    1/4.07|   9.39639|
|         2|       226|    1/5.78|   7.85229|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8234.67 m^2.
Area projection in the x-plane = 668.083 m^2, y-plane = 415.155 m^2, z-plane = 3916.84 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 50 m, y-direction = -97.6729 m, z-direction = -8.4717 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.2566e-01|    1.778264|    4.052124|    3.540124|    7.247370|    0.973936|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2426e-01|    4.266331|    6.508794|    6.312424|    9.744623|    1.276334|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2572e-01|    4.694136|    6.868432|    6.719019|   10.169102|    1.712250|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2470e-01|    4.759562|    7.133453|    7.156909|   10.229087|    2.077370|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2360e-01|    5.227682|    7.724181|    7.671986|   10.709910|    2.715222|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       5.22768|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticIterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file                           |surface_flow_aeroelasticIterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary                     |flow_aeroelasticIterative.szplt    |

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticIterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


==> Running SU2 post-analysis...

==> Running ASTROS pre-analysis...
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = wingSpar1, index = 1
	Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes    = 425
Number of elements = 482
Number of triangle elements      = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes    = 425
Total number of elements = 482
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 4
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2
	Name = leftPointLoad, index = 3
	Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 4
	Name = upperWing, index = 1
	Name = lowerWing, index = 2
	Name = leftTip, index = 3
	Name = riteTip, index = 4
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 = 5
	Name = leftWingSkin, index = 1
	Name = wingRib, index = 2
	Name = riteWingSkin, index = 3
	Name = wingSpar1, index = 4
	Name = wingSpar2, index = 5
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 425
	Number of elements = 482
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 5
	Property name - leftWingSkin
	Property name - riteWingSkin
	Property name - wingRib
	Property name - wingSpar1
	Property name - wingSpar2
	Done getting FEA properties
Updating mesh element types based on properties input

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - rootConstraint
	No "constraintType" specified for Constraint tuple rootConstraint, 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 - pressureAero
	No "groupName" specified for Load tuple pressureAero, going to use load name
	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
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
            Rank 0: src = 2.672164e+12, tgt = 2.672164e+12, diff = 1.047939e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
            Rank 0: src = 2.593437e+12, tgt = 2.593437e+12, diff = 8.613745e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.633345e+08, tgt = 8.633344e+08, diff = 7.283864e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.635510e+08, tgt = 8.635511e+08, diff = 1.545147e+02
Extracting external pressure loads from data transfer....
	TransferName = upperWing
	Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
	TransferName = lowerWing
	Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
	TransferName = leftTip
	Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
	TransferName = riteTip
	Number of Elements = 17 (total = 230)

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
	Writing coordinate system cards

==> Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

==> Running ASTROS post-analysis...

==> Running SU2 pre-analysis...
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"

==> Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Mesh Deformation Code)                     |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2

---------------- Grid deformation parameters ( Zone 0 )  ----------------
Grid deformation using a linear elasticity method.


-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2. 
Cell stiffness scaled by distance to nearest solid surface.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
5317 grid points.
13830 volume elements.
2 surface markers.
9846 boundary elements in index 0 (Marker = BC_1).
12 boundary elements in index 1 (Marker = BC_2).
13830 tetrahedra.

----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 5.96352e+10.
  Info: Ignoring the following volume output fields/groups:
  SOLUTION
Volume output fields: COORDINATES
  Info: Ignoring the following screen output fields:
  RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
  Info: Ignoring the following history output groups:
  RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.

--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.

------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.

WARNING: Convexity is not checked for 3D elements (issue #1171).


Completed in 0.330321 seconds on 1 core.

----------------------- Write deformed grid files -----------------------
|SU2 mesh                           |../aflr3/aflr3_CAPS.su2            |
|CSV file                           |surface_deformed.csv               |
|Tecplot binary                     |volume_deformed.szplt              |
|Tecplot binary surface             |surface_deformed.szplt             |
Adding any FFD information to the SU2 file.

------------------------- Finalize Solver -------------------------
Deleted CNumerics container.
Deleted CSolver container.
Deleted CGeometry container.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted COutput class.

------------------------- Exit Success (SU2_DEF) ------------------------


-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.

Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_2|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
5317 grid points.
13830 volume elements.
2 surface markers.
9846 boundary elements in index 0 (Marker = BC_1).
12 boundary elements in index 1 (Marker = BC_2).
13830 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 5917 TETRAHEDRON volume elements.
There has been a re-orientation of 4468 TRIANGLE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 6.00342e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 37.3071. Mean K: 1.74078. Standard deviation K: 2.28541.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|       0.516955|        78.9368|
|     CV Face Area Aspect Ratio|        1.30468|     5.8651e+06|
|           CV Sub-Volume Ratio|        1.08274|    8.83199e+09|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      5317|    1/1.00|        10|
|         1|      1323|    1/4.02|   9.43457|
|         2|       220|    1/6.01|   7.78218|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 122.669 m.
Wetted area = 632464 m^2.
Area projection in the x-plane = 294887 m^2, y-plane = 82010.6 m^2, z-plane = 33419.1 m^2.
Max. coordinate in the x-direction = 167.237 m, y-direction = 122.669 m, z-direction = 271.513 m.
Min. coordinate in the x-direction = 44.3948 m, y-direction = -125.872 m, z-direction = -460.969 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        211798|             1|   m^2/s^2|        211798|
|            Velocity-X|       100.087|             1|       m/s|       100.087|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|             0|             1|       m/s|             0|
|    Velocity Magnitude|       100.087|             1|       m/s|       100.087|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|      0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  1.5684e-01|    6.555381|    9.522203|    9.454807|   12.024487|   -0.098630|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.5074e-01|    7.262741|    9.654694|    9.723569|   12.765172|    0.076010|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.4457e-01|    7.170902|    9.794731|    9.769565|   12.690244|    0.272611|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.4928e-01|    7.735267|   10.094799|   10.177076|   13.152018|    0.910745|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.5336e-01|    7.315544|    9.967883|    9.850940|   13.042115|   -0.902591|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       7.31554|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_aeroelasticIterative.dat|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file                           |surface_flow_aeroelasticIterative.csv|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary                     |flow_aeroelasticIterative.szplt    |

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface             |surface_flow_aeroelasticIterative.szplt|

Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 1067 non-physical points in the solution.
Warning: 565 reconstructed states for upwinding are non-physical.

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------


==> Running SU2 post-analysis...

==> Running ASTROS pre-analysis...
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
            Rank 0: src = 1.566709e+12, tgt = 1.566709e+12, diff = 3.276406e+02
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
            Rank 0: src = 1.382698e+12, tgt = 1.382698e+12, diff = 1.450830e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
            Rank 0: src = 4.329146e+08, tgt = 4.329146e+08, diff = 3.918651e+01
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
	Number of variables = 16
	Number of data points = 4925
 CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
            Rank 0: src = 8.274979e+08, tgt = 8.274982e+08, diff = 3.115343e+02
Extracting external pressure loads from data transfer....
	TransferName = upperWing
	Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
	TransferName = lowerWing
	Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
	TransferName = leftTip
	Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
	TransferName = riteTip
	Number of Elements = 17 (total = 230)

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
	Writing coordinate system cards

==> Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL

==> Running ASTROS post-analysis...

real	0m43.061s
user	0m48.745s
sys	0m22.703s
+ status=0
+ set +x

=================================================
data/session10/2_aeroelastic_Iterative_SU2_Astros.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

session08 fun3d
session10 nastran
session10 tacs
session11 fun3d+astros
=================================================
=================================================
Summary of examples NOT finished as expected

data/session04/5_mses_OpenMDAO_CD_camber.py

See training.log for more details.
=================================================

=================================================
=================================================
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE