Console Output

Skipping 535 KB.. Full Log
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.5278e-02|    2.467641|    4.648647|    5.247837|    7.945567|  -20.801857|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.5583e-02|    2.558251|    4.773737|    5.362576|    8.081337|   -6.326538|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.5807e-02|    2.693027|    4.777593|    5.517728|    8.240654|   -3.360238|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.5870e-02|    2.804352|    4.865434|    5.634638|    8.340611|    5.845845|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.5690e-02|    2.882515|    4.894916|    5.731159|    8.459787|    0.958965|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.5911e-02|    2.892429|    5.000190|    5.749228|    8.482395|    1.689841|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.89243|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 798 more values.0: Error finishing Tecplot file output.
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
Warning: there are 162 non-physical points in the solution.
Warning: 184 reconstructed states for upwinding are non-physical.

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  0.366395 Cd =  0.216822
Cmz =  0.31747
Cx =  0.216822 Cy =  0.366395
Pressure Contribution
Cl_p =  0.366395 Cd_p =  0.216822
Cmz_p =  0.31747
Cx_p =  0.216822 Cy_p =  0.366395
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m3.334s
user	0m3.079s
sys	0m1.034s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

EGADS    : Face Neighbor-Faces Information

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

EGADS    :   Face          Body   IER       ER    Scale   Neighbor
EGADS    :     ID  Active    ID  Flag   Weight   Factor   Faces
EGADS    :      1     Yes     0     1        1        1   2 3 4 5
EGADS    :      2     Yes     0     1        1        1   1 3 4 6
EGADS    :      3     Yes     0     1        1        1   1 2 4 7
EGADS    :      4     Yes     0     1        1        1   1 2 3
EGADS    :      5     Yes     0     1        1        1   1 6 7 8
EGADS    :      6     Yes     0     1        1        1   2 5 7 8
EGADS    :      7     Yes     0     1        1        1   3 5 6 8
EGADS    :      8     Yes     0     1        1        1   5 6 7
EGADS    :      9     Yes     1     1        0       10   10 11 12 13
EGADS    :     10     Yes     1     1        0       10   9 11 12 14
EGADS    :     11     Yes     1     1        0       10   9 10 12 15
EGADS    :     12     Yes     1     1        0       10   9 10 11
EGADS    :     13     Yes     1     1        0       10   9 14 15 16
EGADS    :     14     Yes     1     1        0       10   10 13 15 16
EGADS    :     15     Yes     1     1        0       10   11 13 14 16
EGADS    :     16     Yes     1     1        0       10   13 14 15
EGADS    :     17     Yes     2     1       NA       NA   18
EGADS    :     18     Yes     2     1       NA       NA   17

EGADS    : Face Edges Information

EGADS    :   Face   Edges
EGADS    :      1   1 4 -3 -2
EGADS    :      2   3 7 -6 -5
EGADS    :      3   6 9 -1 -8
EGADS    :      4   -4 -9 -7
EGADS    :      5   -10 2 11 -12
EGADS    :      6   -11 5 13 -14
EGADS    :      7   -13 8 10 -15
EGADS    :      8   12 14 15
EGADS    :      9   16 19 -18 -17
EGADS    :     10   18 22 -21 -20
EGADS    :     11   21 24 -16 -23
EGADS    :     12   -19 -24 -22
EGADS    :     13   -25 17 26 -27
EGADS    :     14   -26 20 28 -29
EGADS    :     15   -28 23 25 -30
EGADS    :     16   27 29 30
EGADS    :     17   -31 -32 33 34
EGADS    :     18   -35 -34 36 32

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    :     17   17
EGADS    :     18   18

EGADS    : Loop Edges Information

EGADS    :   Loop  Active Sense   Edges
EGADS    :      1     Yes     1   1 4 -3 -2
EGADS    :      2     Yes     1   3 7 -6 -5
EGADS    :      3     Yes     1   6 9 -1 -8
EGADS    :      4     Yes     1   -4 -9 -7
EGADS    :      5     Yes     1   -10 2 11 -12
EGADS    :      6     Yes     1   -11 5 13 -14
EGADS    :      7     Yes     1   -13 8 10 -15
EGADS    :      8     Yes     1   12 14 15
EGADS    :      9     Yes     1   16 19 -18 -17
EGADS    :     10     Yes     1   18 22 -21 -20
EGADS    :     11     Yes     1   21 24 -16 -23
EGADS    :     12     Yes     1   -19 -24 -22
EGADS    :     13     Yes     1   -25 17 26 -27
EGADS    :     14     Yes     1   -26 20 28 -29
EGADS    :     15     Yes     1   -28 23 25 -30
EGADS    :     16     Yes     1   27 29 30
EGADS    :     17     Yes     1   -31 -32 33 34
EGADS    :     18     Yes     1   -35 -34 36 32

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 5
EGADS    :      3     0     Yes     3     4        1   1 2
EGADS    :      4     0     Yes     2     4        1   1 4
EGADS    :      5     0     Yes     3     5        1   2 6
EGADS    :      6     0     Yes     5     6        1   2 3
EGADS    :      7     0     Yes     4     6        1   2 4
EGADS    :      8     0     Yes     5     1        1   3 7
EGADS    :      9     0     Yes     6     2        1   3 4
EGADS    :     10     0     Yes     1     7        1   5 7
EGADS    :     11     0     Yes     3     8        1   5 6
EGADS    :     12     0     Yes     7     8        1   5 8
EGADS    :     13     0     Yes     5     9        1   6 7
EGADS    :     14     0     Yes     8     9        1   6 8
EGADS    :     15     0     Yes     9     7        1   7 8
EGADS    :     16     1     Yes    10    11        1   9 11
EGADS    :     17     1     Yes    10    12        1   9 13
EGADS    :     18     1     Yes    12    13        1   9 10
EGADS    :     19     1     Yes    11    13        1   9 12
EGADS    :     20     1     Yes    12    14        1   10 14
EGADS    :     21     1     Yes    14    15        1   10 11
EGADS    :     22     1     Yes    13    15        1   10 12
EGADS    :     23     1     Yes    14    10        1   11 15
EGADS    :     24     1     Yes    15    11        1   11 12
EGADS    :     25     1     Yes    10    16        1   13 15
EGADS    :     26     1     Yes    12    17        1   13 14
EGADS    :     27     1     Yes    16    17        1   13 16
EGADS    :     28     1     Yes    14    18        1   14 15
EGADS    :     29     1     Yes    17    18        1   14 16
EGADS    :     30     1     Yes    18    16        1   15 16
EGADS    :     31     2   Degen    19    19        -   17
EGADS    :     32     2     Yes    20    19       NA   17 18
EGADS    :     33     2   Degen    20    20        -   17
EGADS    :     34     2     Yes    20    19       NA   17 18
EGADS    :     35     2   Degen    19    19        -   18
EGADS    :     36     2   Degen    20    20        -   18

EGADS    : Node Information

EGADS    :   Node  Active      Coordinates
EGADS    :      1     Yes       4.21773908                0    0.00513324532
EGADS    :      2     Yes       6.60185093       7.90569415                0
EGADS    :      3     Yes                0                0                0
EGADS    :      4     Yes       4.56435465       7.90569415      0.137994405
EGADS    :      5     Yes       4.21500135                0                0
EGADS    :      6     Yes       6.59955925       7.90569415                0
EGADS    :      7     Yes       6.60185093                0                0
EGADS    :      8     Yes       4.56435465                0      0.137994405
EGADS    :      9     Yes       6.59955925                0                0
EGADS    :     10     Yes       11.6870956                0    0.00205329813
EGADS    :     11     Yes       12.6407404       3.16227766                0
EGADS    :     12     Yes               10                0                0
EGADS    :     13     Yes       11.8257419       3.16227766     0.0551977619
EGADS    :     14     Yes       11.6860005                0                0
EGADS    :     15     Yes       12.6398237       3.16227766                0
EGADS    :     16     Yes       12.6407404                0                0
EGADS    :     17     Yes       11.8257419                0     0.0551977619
EGADS    :     18     Yes       12.6398237                0                0
EGADS    :     19     Yes                0                0               80
EGADS    :     20     Yes                0                0                0
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

Writing TECPLOT file: AFLR4_Mesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: AFLR4_Mesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: AFLR4_Mesh_Surf_2.dat ....
Finished writing TECPLOT file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface nodes - 6280
Number of surface elements - 12548
Getting volume mesh
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.31.6
AFLR3    : Version Date   08/30/21 @ 12:37AM
AFLR3    : Compile OS     Darwin 19.6.0 x86_64
AFLR3    : Compile Date   08/30/21 @ 12:37AM
AFLR3    : Copyright 1994-2021, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6280         0

UG3      : Boundary Conditions

UG3      :  B-Face ID            Boundary Condition
UG3      :          1                      FarField
UG3      :          2                      FarField
UG3      :          3                      FarField
 
AFLR3    : CPU Time          =     0.011   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6280         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1258      7861
AFLR3 IG : Nodes, Elements   =      2516     16467
AFLR3 IG : Nodes, Elements   =      3774     25140
AFLR3 IG : Nodes, Elements   =      5032     34337
AFLR3 IG : Nodes, Elements   =      6287     43428
AFLR3 IG : Nodes, Elements   =      6287     43354
AFLR3 IG : Nodes, Elements   =      6280     25660
AFLR3 IG : Nodes, Elements   =      6280     25675
AFLR3 IG : Nodes, Elements   =      6280     20287
AFLR3 IG : Nodes, Elements   =      6280     18341
 
AFLR3    : CPU Time          =     0.126   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6280     18341
AFLR3 GG : Nodes, Elements   =      9221     27366
AFLR3 GG : Nodes, Elements   =      9221     39962
AFLR3 GG : Nodes, Elements   =      9221     36588
AFLR3 GG : Nodes, Elements   =      9221     35182
AFLR3 GG : Nodes, Elements   =     11840     43393
AFLR3 GG : Nodes, Elements   =     11840     54847
AFLR3 GG : Nodes, Elements   =     11840     51719
AFLR3 GG : Nodes, Elements   =     11840     50960
AFLR3 GG : Nodes, Elements   =     14664     59670
AFLR3 GG : Nodes, Elements   =     14664     71755
AFLR3 GG : Nodes, Elements   =     14664     68346
AFLR3 GG : Nodes, Elements   =     14664     67551
AFLR3 GG : Nodes, Elements   =     17705     76837
AFLR3 GG : Nodes, Elements   =     17705     89934
AFLR3 GG : Nodes, Elements   =     17705     86464
AFLR3 GG : Nodes, Elements   =     17705     85581
AFLR3 GG : Nodes, Elements   =     20867     95251
AFLR3 GG : Nodes, Elements   =     20867    108813
AFLR3 GG : Nodes, Elements   =     20867    105088
AFLR3 GG : Nodes, Elements   =     20867    104279
AFLR3 GG : Nodes, Elements   =     24207    114449
AFLR3 GG : Nodes, Elements   =     24207    128677
AFLR3 GG : Nodes, Elements   =     24207    124813
AFLR3 GG : Nodes, Elements   =     24207    124013
AFLR3 GG : Nodes, Elements   =     27639    134423
AFLR3 GG : Nodes, Elements   =     27639    149008
AFLR3 GG : Nodes, Elements   =     27639    145234
AFLR3 GG : Nodes, Elements   =     27639    144424
AFLR3 GG : Nodes, Elements   =     31166    155093
AFLR3 GG : Nodes, Elements   =     31166    170090
AFLR3 GG : Nodes, Elements   =     31166    166194
AFLR3 GG : Nodes, Elements   =     31166    165380
AFLR3 GG : Nodes, Elements   =     34680    175992
AFLR3 GG : Nodes, Elements   =     34680    190960
AFLR3 GG : Nodes, Elements   =     34680    186974
AFLR3 GG : Nodes, Elements   =     34680    186209
AFLR3 GG : Nodes, Elements   =     38121    196595
AFLR3 GG : Nodes, Elements   =     38121    211142
AFLR3 GG : Nodes, Elements   =     38121    207406
AFLR3 GG : Nodes, Elements   =     38121    206612
AFLR3 GG : Nodes, Elements   =     41440    216611
AFLR3 GG : Nodes, Elements   =     41440    230632
AFLR3 GG : Nodes, Elements   =     41440    227051
AFLR3 GG : Nodes, Elements   =     41440    226371
AFLR3 GG : Nodes, Elements   =     44725    236250
AFLR3 GG : Nodes, Elements   =     44725    250090
AFLR3 GG : Nodes, Elements   =     44725    246576
AFLR3 GG : Nodes, Elements   =     44725    245969
AFLR3 GG : Nodes, Elements   =     47816    255261
AFLR3 GG : Nodes, Elements   =     47816    268274
AFLR3 GG : Nodes, Elements   =     47816    264971
AFLR3 GG : Nodes, Elements   =     47816    264363
AFLR3 GG : Nodes, Elements   =     50812    273367
AFLR3 GG : Nodes, Elements   =     50812    285946
AFLR3 GG : Nodes, Elements   =     50812    282825
AFLR3 GG : Nodes, Elements   =     50812    282276
AFLR3 GG : Nodes, Elements   =     53664    290847
AFLR3 GG : Nodes, Elements   =     53664    302853
AFLR3 GG : Nodes, Elements   =     53664    299809
AFLR3 GG : Nodes, Elements   =     53664    299303
AFLR3 GG : Nodes, Elements   =     56368    307422
AFLR3 GG : Nodes, Elements   =     56368    318735
AFLR3 GG : Nodes, Elements   =     56368    315890
AFLR3 GG : Nodes, Elements   =     56368    315469
AFLR3 GG : Nodes, Elements   =     58879    323008
AFLR3 GG : Nodes, Elements   =     58879    333588
AFLR3 GG : Nodes, Elements   =     58879    330877
AFLR3 GG : Nodes, Elements   =     58879    330488
AFLR3 GG : Nodes, Elements   =     61072    337073
AFLR3 GG : Nodes, Elements   =     61072    346408
AFLR3 GG : Nodes, Elements   =     61072    343977
AFLR3 GG : Nodes, Elements   =     61072    343661
AFLR3 GG : Nodes, Elements   =     62995    349431
AFLR3 GG : Nodes, Elements   =     62995    357483
AFLR3 GG : Nodes, Elements   =     62995    355435
AFLR3 GG : Nodes, Elements   =     62995    355166
AFLR3 GG : Nodes, Elements   =     64589    359949
AFLR3 GG : Nodes, Elements   =     64589    366686
AFLR3 GG : Nodes, Elements   =     64589    364912
AFLR3 GG : Nodes, Elements   =     64589    364688
AFLR3 GG : Nodes, Elements   =     65843    368453
AFLR3 GG : Nodes, Elements   =     65843    373910
AFLR3 GG : Nodes, Elements   =     65843    372416
AFLR3 GG : Nodes, Elements   =     65843    372250
AFLR3 GG : Nodes, Elements   =     66821    375185
AFLR3 GG : Nodes, Elements   =     66821    379253
AFLR3 GG : Nodes, Elements   =     66821    378165
AFLR3 GG : Nodes, Elements   =     66821    378049
AFLR3 GG : Nodes, Elements   =     67498    380080
AFLR3 GG : Nodes, Elements   =     67498    382986
AFLR3 GG : Nodes, Elements   =     67498    382160
AFLR3 GG : Nodes, Elements   =     67498    382082
AFLR3 GG : Nodes, Elements   =     67927    383370
AFLR3 GG : Nodes, Elements   =     67927    385253
AFLR3 GG : Nodes, Elements   =     67927    384714
AFLR3 GG : Nodes, Elements   =     67927    384664
AFLR3 GG : Nodes, Elements   =     68142    385309
AFLR3 GG : Nodes, Elements   =     68142    386224
AFLR3 GG : Nodes, Elements   =     68142    385951
AFLR3 GG : Nodes, Elements   =     68142    385928
AFLR3 GG : Nodes, Elements   =     68246    386240
AFLR3 GG : Nodes, Elements   =     68246    386726
AFLR3 GG : Nodes, Elements   =     68246    386570
AFLR3 GG : Nodes, Elements   =     68246    386554
AFLR3 GG : Nodes, Elements   =     68293    386695
AFLR3 GG : Nodes, Elements   =     68293    386899
AFLR3 GG : Nodes, Elements   =     68293    386838
AFLR3 GG : Nodes, Elements   =     68293    386833
AFLR3 GG : Nodes, Elements   =     68314    386896
AFLR3 GG : Nodes, Elements   =     68314    387005
AFLR3 GG : Nodes, Elements   =     68314    386956
AFLR3 GG : Nodes, Elements   =     68314    386954
AFLR3 GG : Nodes, Elements   =     68321    386975
AFLR3 GG : Nodes, Elements   =     68321    387013
AFLR3 GG : Nodes, Elements   =     68321    386998
AFLR3 GG : Nodes, Elements   =     68323    387004
AFLR3 GG : Nodes, Elements   =     68323    387012
AFLR3 GG : Nodes, Elements   =     68323    387009
AFLR3 GG : Nodes, Elements   =     68355    387105
AFLR3 GG : Nodes, Elements   =     68355    387227
AFLR3 GG : Nodes, Elements   =     68355    387184
AFLR3 GG : Nodes, Elements   =     68355    387190
AFLR3 GG : Nodes, Elements   =     68359    387202
AFLR3 GG : Nodes, Elements   =     68359    387214
AFLR3 GG : Nodes, Elements   =     68359    387210
AFLR3 GG : Nodes, Elements   =     68359    387211
 
AFLR3    : CPU Time          =     3.976   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     68359    387211
AFLR3 QI : Nodes, Elements   =     66997    379472
AFLR3 QI : Nodes, Elements   =     66810    378427
AFLR3 QI : Nodes, Elements   =     66798    378359
AFLR3 QI : Nodes, Elements   =     66798    382090
AFLR3 QI : Nodes, Elements   =     66798    378114
AFLR3 QI : Nodes, Elements   =     66798    377728
AFLR3 QI : Nodes, Elements   =     66798    378120
AFLR3 QI : Nodes, Elements   =     66798    377487
AFLR3 QI : Nodes, Elements   =     66798    377277
AFLR3 QI : Nodes, Elements   =     66798    377596
AFLR3 QI : Nodes, Elements   =     66798    377253
AFLR3 QI : Nodes, Elements   =     66798    377157
AFLR3 QI : Nodes, Elements   =     66798    377466
AFLR3 QI : Nodes, Elements   =     66798    377172
AFLR3 QI : Nodes, Elements   =     66798    377128
AFLR3 QI : Nodes, Elements   =     66798    377452
AFLR3 QI : Nodes, Elements   =     66798    377141
AFLR3 QI : Nodes, Elements   =     66798    377097
AFLR3 QI : Nodes, Elements   =     66804    377122
AFLR3 QI : Nodes, Elements   =     66804    377427
AFLR3 QI : Nodes, Elements   =     66804    377147
AFLR3 QI : Nodes, Elements   =     66804    377127
AFLR3 QI : Nodes, Elements   =     66804    377430
AFLR3 QI : Nodes, Elements   =     66804    377146
AFLR3 QI : Nodes, Elements   =     66804    377115
AFLR3 QI : Nodes, Elements   =     66804    377122
 
AFLR3    : CPU Time          =     1.499   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     66804    377122
AFLR3 QRG: Nodes, Elements   =     66806    377132
AFLR3 QRG: Nodes, Elements   =     66814    377173
AFLR3 QRG: Nodes, Elements   =     66814    377174
AFLR3 QRG: Nodes, Elements   =     66827    377242
AFLR3 QRG: Nodes, Elements   =     66826    377243
 
AFLR3    : CPU Time          =     0.043   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    377243
UG3      : Min, Max Ang      =     1.153     169.2
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        48
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.08e+06

UG3      : No. Tet Elems     =    377243
UG3      : Min Vol           =  9.64e-10
UG3      : Average Vol       =      5.53
UG3      : Total-Tet-Vol     =  2.08e+06
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     =    377243
UG3      : Min, Max Q        =    0.0821         1
UG3      : Average Q         =     0.891
UG3      : No. Q<       0.1  =        23
UG3      : No. Q<      0.01  =         0
Volume mesh:
	Number of nodes = 66826
	Number of elements = 389791
	Number of triangles = 12548
	Number of quadrilatarals = 0
	Number of tetrahedrals = 377243
	Number of pyramids= 0
	Number of prisms= 0
	Number of hexahedrals= 0

Writing TECPLOT file: AFLR3_Mesh.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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: 0.5901.
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 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_0.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 ) ----------------------
Writing solution files every 250 iterations.
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_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_3|
+-----------------------------------------------------------------------+
|                     Heat flux wall|                               BC_1|
+-----------------------------------------------------------------------+

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

WARNING: SURFACE_PRESSURE_DROP can only be computed for 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.
66826 grid points.
377243 volume elements.
3 surface markers.
6726 boundary elements in index 0 (Marker = BC_1).
5418 boundary elements in index 1 (Marker = BC_2).
404 boundary elements in index 2 (Marker = BC_3).
377243 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: 2.08442e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4867.4. Mean K: 61.8717. Standard deviation K: 268.151.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        41.9341|        86.3983|
|     CV Face Area Aspect Ratio|         1.1644|        63.4315|
|           CV Sub-Volume Ratio|        1.07219|        522.696|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     66826|    1/1.00|        10|
|         1|     10893|    1/6.13|   8.19392|
|         2|      1641|    1/6.64|   6.53989|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.039 m^2.
Area projection in the x-plane = 11.1556 m^2, y-plane = 4.97851 m^2, z-plane = 55.3964 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_2 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|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.1321e+00|   -0.182790|    2.584316|    2.095841|    5.308105|    4.670017|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.1501e+00|    0.092451|    2.664168|    2.260050|    5.597552|   23.149469|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0921e+00|    0.135596|    2.694342|    2.395513|    5.642260|   -8.220456|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.1114e+00|    0.128028|    2.678731|    2.470623|    5.633419|   -4.383061|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.0996e+00|    0.156443|    2.652503|    2.486627|    5.653026|   -3.579778|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  2.1211e+00|    0.172282|    2.630559|    2.513510|    5.666233|   -3.669320|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  2.1014e+00|    0.176848|    2.622987|    2.548153|    5.664093|   -4.939530|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  2.0917e+00|    0.204505|    2.632818|    2.561118|    5.688402|   -7.191285|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  2.1106e+00|    0.267900|    2.680775|    2.577764|    5.740992|   -9.863069|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  2.1061e+00|    0.368079|    2.773797|    2.641181|    5.840253|   -9.742028|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.368079|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |
|CSV file                           |surface_flow_su2AFLRTest.csv       |
|Paraview                           |flow_su2AFLRTest.vtu               |
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
Warning: there are 9 non-physical points in the solution.
Warning: 101 reconstructed states for upwinding are non-physical.

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  1.309174 Cd =  -0.134384
Cmx =  8e-06 Cmy =  -0.359602 Cmz =  0.005618
Cx =  -0.157212 Cy =  0.005828 Cz =  1.30663
Pressure Contribution
Cl_p =  1.309174 Cd_p =  -0.134384
Cmx_p =  8e-06 Cmy_p =  -0.359602 Cmz_p =  0.005618
Cx_p =  -0.157212 Cy_p =  0.005828 Cz_p =  1.30663
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0

real	0m37.633s
user	0m35.958s
sys	0m1.304s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5

Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes be in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundoMesh.mesh
	Swapping y and z coordinates!

Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file


Writing SU2 file ....
SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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: 0.4.
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 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.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-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
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_delaundoMesh.dat.
Surface file name: surface_flow_delaundoMesh.
Volume file name: flow_delaundoMesh.
Restart file name: restart_flow_delaundoMesh.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

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

WARNING: SURFACE_PRESSURE_DROP can only be computed for 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 ) -------------------
Two dimensional problem.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
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.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        45.3524|        89.3051|
|     CV Face Area Aspect Ratio|         1.0235|        15.7138|
|           CV Sub-Volume Ratio|              1|        7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      6320|    1/1.00|        10|
|         1|      1790|    1/3.53|   7.98287|
|         2|       504|    1/3.55|   6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
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|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  6.5562e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  6.4681e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  6.4135e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  6.4703e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  6.4961e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  6.5226e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  6.5535e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349556|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  6.5836e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104876|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  6.5774e-02|   -1.659565|    1.020774|    0.939260|    3.804303|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  6.5689e-02|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456835|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.67676|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_delaundoMesh.dat      |
|CSV file                           |surface_flow_delaundoMesh.csv      |
|Tecplot binary                     |flow_delaundoMesh.szplt            |
|Tecplot binary surface             |surface_flow_delaundoMesh.szplt    |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  0.805231 Cd =  -0.037528
Cmz =  0.414714
Cx =  -0.037528 Cy =  0.805231
Pressure Contribution
Cl_p =  0.805231 Cd_p =  -0.037528
Cmz_p =  0.414714
Cx_p =  -0.037528 Cy_p =  0.805231
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m2.690s
user	0m2.505s
sys	0m0.725s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_pointwise_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Number of command line arguments = 2
Sat Jun 11 2022  6:42:38AM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 10
    MaxDim                   = 15
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 18 entries.
  Quilt quilt-1: edge tolerance = 6.19984e-05
  Quilt quilt-2: edge tolerance = 6.19984e-05
  Quilt quilt-3: edge tolerance = 6.19984e-05
  Quilt quilt-4: edge tolerance = 6.19984e-05
  Quilt quilt-5: edge tolerance = 6.19984e-05
  Quilt quilt-6: edge tolerance = 6.19984e-05
  Quilt quilt-7: edge tolerance = 6.19984e-05
  Quilt quilt-8: edge tolerance = 6.19984e-05
  Quilt quilt-9: edge tolerance = 8.32902e-05
  Quilt quilt-10: edge tolerance = 8.32902e-05
  Quilt quilt-11: edge tolerance = 8.32902e-05
  Quilt quilt-12: edge tolerance = 8.32902e-05
  Quilt quilt-13: edge tolerance = 8.32902e-05
  Quilt quilt-14: edge tolerance = 8.32902e-05
  Quilt quilt-15: edge tolerance = 8.32902e-05
  Quilt quilt-16: edge tolerance = 8.32902e-05
  Quilt quilt-17: edge tolerance = 6.19601e-06
  Quilt quilt-18: edge tolerance = 6.19601e-06
  Maximum DB edge tolerance = 8.32902e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.665804e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 18 entries.
Quilt list has 18 entries.
Original connector list has 32 entries.
Minimum connector length = 0.00316783
Tolerance = 8.32902e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 32 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-12
Max Edge Tol: 8.329e-05 on con-23
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/32, name = con-1
  Changing dimension for connector 1/32 from 10 to 4
Checking dimension for connector 2/32, name = con-2
Checking dimension for connector 3/32, name = con-3
  Changing dimension for connector 3/32 from 10 to 3
Checking dimension for connector 4/32, name = con-4
Checking dimension for connector 5/32, name = con-5
  Changing dimension for connector 5/32 from 10 to 3
Checking dimension for connector 6/32, name = con-6
  Changing dimension for connector 6/32 from 10 to 3
Checking dimension for connector 7/32, name = con-7
  Changing dimension for connector 7/32 from 10 to 3
Checking dimension for connector 8/32, name = con-8
Checking dimension for connector 9/32, name = con-9
  Changing dimension for connector 9/32 from 10 to 4
Checking dimension for connector 10/32, name = con-10
Checking dimension for connector 11/32, name = con-12
  Changing dimension for connector 11/32 from 10 to 3
Checking dimension for connector 12/32, name = con-13
Checking dimension for connector 13/32, name = con-16
  Changing dimension for connector 13/32 from 10 to 3
Checking dimension for connector 14/32, name = con-17
Checking dimension for connector 15/32, name = con-20
  Changing dimension for connector 15/32 from 10 to 3
Checking dimension for connector 16/32, name = con-21
  Changing dimension for connector 16/32 from 10 to 4
Checking dimension for connector 17/32, name = con-22
Checking dimension for connector 18/32, name = con-23
  Changing dimension for connector 18/32 from 10 to 3
Checking dimension for connector 19/32, name = con-24
Checking dimension for connector 20/32, name = con-25
  Changing dimension for connector 20/32 from 10 to 3
Checking dimension for connector 21/32, name = con-26
  Changing dimension for connector 21/32 from 10 to 3
Checking dimension for connector 22/32, name = con-27
  Changing dimension for connector 22/32 from 10 to 3
Checking dimension for connector 23/32, name = con-28
Checking dimension for connector 24/32, name = con-29
  Changing dimension for connector 24/32 from 10 to 4
Checking dimension for connector 25/32, name = con-30
Checking dimension for connector 26/32, name = con-32
  Changing dimension for connector 26/32 from 10 to 3
Checking dimension for connector 27/32, name = con-33
Checking dimension for connector 28/32, name = con-36
  Changing dimension for connector 28/32 from 10 to 3
Checking dimension for connector 29/32, name = con-37
Checking dimension for connector 30/32, name = con-40
  Changing dimension for connector 30/32 from 10 to 3
Checking dimension for connector 31/32, name = con-41
Checking dimension for connector 32/32, name = con-42
Processing spacing values for connector 1/32, name = con-1
Processing spacing values for connector 2/32, name = con-2
Processing spacing values for connector 3/32, name = con-3
Processing spacing values for connector 4/32, name = con-4
Processing spacing values for connector 5/32, name = con-5
Processing spacing values for connector 6/32, name = con-6
Processing spacing values for connector 7/32, name = con-7
Processing spacing values for connector 8/32, name = con-8
Processing spacing values for connector 9/32, name = con-9
Processing spacing values for connector 10/32, name = con-10
Processing spacing values for connector 11/32, name = con-12
Processing spacing values for connector 12/32, name = con-13
Processing spacing values for connector 13/32, name = con-16
Processing spacing values for connector 14/32, name = con-17
Processing spacing values for connector 15/32, name = con-20
Processing spacing values for connector 16/32, name = con-21
Processing spacing values for connector 17/32, name = con-22
Processing spacing values for connector 18/32, name = con-23
Processing spacing values for connector 19/32, name = con-24
Processing spacing values for connector 20/32, name = con-25
Processing spacing values for connector 21/32, name = con-26
Processing spacing values for connector 22/32, name = con-27
Processing spacing values for connector 23/32, name = con-28
Processing spacing values for connector 24/32, name = con-29
Processing spacing values for connector 25/32, name = con-30
Processing spacing values for connector 26/32, name = con-32
Processing spacing values for connector 27/32, name = con-33
Processing spacing values for connector 28/32, name = con-36
Processing spacing values for connector 29/32, name = con-37
Processing spacing values for connector 30/32, name = con-40
Processing spacing values for connector 31/32, name = con-41
Processing spacing values for connector 32/32, name = con-42
Number of unique endpoints = 20
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/32, con-1.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.33869 to 0.286862
  Proximity test for connector 2/32, con-2.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 3/32, con-3.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 4/32, con-4.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 5/32, con-5.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 6/32, con-6.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 7/32, con-7.
  Proximity test for connector 8/32, con-8.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 9/32, con-9.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.26705 to 0.271511
  Proximity test for connector 10/32, con-10.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 11/32, con-12.
  Proximity test for connector 12/32, con-13.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 13/32, con-16.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 14/32, con-17.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 15/32, con-20.
  Proximity test for connector 16/32, con-21.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.535476 to 0.114745
  Proximity test for connector 17/32, con-22.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 18/32, con-23.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 19/32, con-24.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 20/32, con-25.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 21/32, con-26.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 22/32, con-27.
  Proximity test for connector 23/32, con-28.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 24/32, con-29.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.506821 to 0.108604
  Proximity test for connector 25/32, con-30.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 26/32, con-32.
  Proximity test for connector 27/32, con-33.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 28/32, con-36.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 29/32, con-37.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 30/32, con-40.
  Proximity test for connector 31/32, con-41.
    Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
  Proximity test for connector 32/32, con-42.
    Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 15
Connector con-2 current dim = 15
Connector con-3 current dim = 15
Connector con-4 current dim = 15
Connector con-5 current dim = 15
Connector con-6 current dim = 15
Connector con-7 current dim = 3
Connector con-8 current dim = 15
Connector con-9 current dim = 15
Connector con-10 current dim = 15
Connector con-12 current dim = 3
Connector con-13 current dim = 15
Connector con-16 current dim = 15
Connector con-17 current dim = 15
Connector con-20 current dim = 3
Connector con-21 current dim = 15
Connector con-22 current dim = 15
Connector con-23 current dim = 15
Connector con-24 current dim = 15
Connector con-25 current dim = 15
Connector con-26 current dim = 15
Connector con-27 current dim = 3
Connector con-28 current dim = 15
Connector con-29 current dim = 15
Connector con-30 current dim = 15
Connector con-32 current dim = 3
Connector con-33 current dim = 15
Connector con-36 current dim = 15
Connector con-37 current dim = 15
Connector con-40 current dim = 3
Connector con-41 current dim = 15
Connector con-42 current dim = 15
Domain list has 18 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 8.32902e-05
Number of periodic target domains = 0
Unstructured domain 1 of 18:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 2 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 3 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 4 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 5 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 6 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 7 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 8 of 18:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 18:
  boundary name = Wing2.
    Creating boundary name Wing2
Unstructured domain 10 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 11 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 12 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 13 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 14 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 15 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 16 of 18:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 17 of 18:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 18 of 18:
  boundary name = Farfield.
    Farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 18 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 18 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Sat Jun 11 2022  6:42:45AM EDT
Run Time: 00 Hours 00 Minutes 07 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Sat Jun 11 2022  6:42:46AM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 96 / 96 curves to EGADS originals
GMA contains 32 edge groups
GMA contains 18 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Sat Jun 11 2022  6:42:48AM EDT
Export Time: 00 Hours 00 Minutes 02 Seconds
Volume mesh:
	Number of nodes          = 16315
	Number of elements       = 95272
	Number of triangles      = 2986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 95272
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 548
	Number of elements = 1092
	Number of tris = 1092
	Number of quad = 0
Body = 2
	Number of nodes    = 556
	Number of elements = 1108
	Number of tris = 1108
	Number of quad = 0
Body = 3
	Number of nodes    = 395
	Number of elements = 786
	Number of tris = 786
	Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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: 0.5901.
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 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_2 (0, 0, 0).
   - BC_3 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_2, BC_3.
Input mesh file name: ../pointwise/caps.GeomToMesh.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 ) ----------------------
Writing solution files every 250 iterations.
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_pyCAPS_SU2_Pointwise.dat.
Surface file name: surface_flow_pyCAPS_SU2_Pointwise.
Volume file name: flow_pyCAPS_SU2_Pointwise.
Restart file name: restart_flow_pyCAPS_SU2_Pointwise.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_2|
|                                   |                               BC_3|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_1|
+-----------------------------------------------------------------------+

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

WARNING: SURFACE_PRESSURE_DROP can only be computed for 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.
16315 grid points.
95272 volume elements.
3 surface markers.
786 boundary elements in index 0 (Marker = BC_1).
1092 boundary elements in index 1 (Marker = BC_2).
1108 boundary elements in index 2 (Marker = BC_3).
95272 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: 2.11302e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 6570.86. Mean K: 103.512. Standard deviation K: 506.754.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        41.2028|        83.6885|
|     CV Face Area Aspect Ratio|        1.14048|        288.283|
|           CV Sub-Volume Ratio|        1.17114|        1683.18|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     16315|    1/1.00|        10|
|         1|      2579|    1/6.33|   8.11047|
|         2|       377|    1/6.84|   6.40866|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 90.089 m^2.
Area projection in the x-plane = 8.32094 m^2, y-plane = 3.6838 m^2, z-plane = 42.3969 m^2.
Max. coordinate in the x-direction = 12.3619 m, y-direction = 7.07107 m, z-direction = 0.510646 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.368435 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_2 is NOT a single plane.
Boundary marker BC_3 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|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  4.7604e-01|    0.438235|    2.854060|    2.414895|    5.929130|    2.172311|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.7262e-01|    0.189651|    2.668076|    2.392003|    5.676489|    2.680595|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.6703e-01|    0.145200|    2.674788|    2.524460|    5.622835|    3.669306|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.6829e-01|    0.077134|    2.671215|    2.589484|    5.552544|    4.794305|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.6782e-01|    0.005877|    2.673133|    2.606260|    5.487738|    5.541684|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|    0.00587703|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Pointwise.dat|
|CSV file                           |surface_flow_pyCAPS_SU2_Pointwise.csv|
|Tecplot binary                     |flow_pyCAPS_SU2_Pointwise.szplt    |
|Tecplot binary surface             |surface_flow_pyCAPS_SU2_Pointwise.szplt|
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  0.64688 Cd =  0.11673
Cmx =  0.002436 Cmy =  -0.191647 Cmz =  8.1e-05
Cx =  0.105422 Cy =  0.000479 Cz =  0.648819

real	0m21.978s
user	0m12.555s
sys	0m2.416s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface nodes - 3139
Number of surface elements - 6266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  0.047801
Creating surface mesh ...
Surface mesh seconds:  0.013088
Recovering boundaries...
Boundary recovery seconds:  0.141717
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.015202
Suppressing Steiner points ...
Steiner suppression seconds:  1.5e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.02759
Refining mesh...
  4189 insertions, added 2138 points, 127097 tetrahedra in queue.
  1394 insertions, added 409 points, 130640 tetrahedra in queue.
  1859 insertions, added 449 points, 127916 tetrahedra in queue.
  2478 insertions, added 473 points, 111923 tetrahedra in queue.
  3303 insertions, added 484 points, 65315 tetrahedra in queue.
  4403 insertions, added 433 points, 571 tetrahedra in queue.
Refinement seconds:  1.50004
Smoothing vertices...
Mesh smoothing seconds:  0.950285
Improving mesh...
Mesh improvement seconds:  0.042413
Jettisoning redundant points.

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

Output seconds:  0.005315
Total running seconds:  2.74398

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 8039
  Mesh tetrahedra: 39668
  Mesh faces: 82470
  Mesh faces on exterior boundary: 6268
  Mesh faces on input facets: 6268
  Mesh edges on input segments: 9400
  Steiner points on input segments:  1
  Steiner points inside domain: 4899

Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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: 0.5901.
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 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and 
their reference origin for moment computation: 
   - BC_1 (0, 0, 0).
   - BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_0.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 ) ----------------------
Writing solution files every 250 iterations.
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_pyCAPS_SU2_Tetgen.dat.
Surface file name: surface_flow_pyCAPS_SU2_Tetgen.
Volume file name: flow_pyCAPS_SU2_Tetgen.
Restart file name: restart_flow_pyCAPS_SU2_Tetgen.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_3|
+-----------------------------------------------------------------------+

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

WARNING: SURFACE_PRESSURE_DROP can only be computed for 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.
8039 grid points.
39668 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39668 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: 2.08934e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.83144|        84.8022|
|     CV Face Area Aspect Ratio|        1.55015|        7101.39|
|           CV Sub-Volume Ratio|        1.05639|         198266|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8039|    1/1.00|        10|
|         1|      1338|    1/6.01|   8.25105|
|         2|       214|    1/6.25|    6.7182|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 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|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  2.1264e-01|    0.619384|    3.051344|    2.094590|    6.110279|    1.812161|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.0826e-01|    0.785542|    3.264371|    2.974872|    6.285549|    2.181906|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.0678e-01|    0.724139|    3.334285|    3.249736|    6.229534|    3.226648|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.0596e-01|    0.621976|    3.305627|    3.334988|    6.113861|    4.648342|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.0523e-01|    0.625390|    3.207240|    3.303991|    6.098630|    5.785533|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       0.62539|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |
|Paraview surface                   |surface_flow_pyCAPS_SU2_Tetgen.vtu |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  0.759441 Cd =  0.131266
Cmx =  0.001646 Cmy =  -0.215157 Cmz =  0.000487
Cx =  0.117991 Cy =  0.00137 Cz =  0.761616

real	3m29.966s
user	3m29.036s
sys	0m0.959s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 3808
Number of elements = 7616
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 5654
Number of elements = 11304
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11304
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9462
Total number of elements = 18920

Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = x43A, index = 1
	Name = Farfield, index = 2
Number of surface nodes - 9462
Number of surface elements - 18920
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  0.145377
Creating surface mesh ...
Surface mesh seconds:  0.038521
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  0.319141
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.022357
Suppressing Steiner points ...
Steiner suppression seconds:  2e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.041524
Refining mesh...
  12618 insertions, added 5266 points, 45 tetrahedra in queue.
Refinement seconds:  1.5351
Smoothing vertices...
Mesh smoothing seconds:  1.14698
Improving mesh...
Mesh improvement seconds:  0.064174
Jettisoning redundant points.

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

Output seconds:  0.01175
Total running seconds:  3.33549

Statistics:

  Input points: 9462
  Input facets: 18920
  Input segments: 28380
  Input holes: 1
  Input regions: 0

  Mesh points: 14871
  Mesh tetrahedra: 61451
  Mesh faces: 132365
  Mesh faces on exterior boundary: 18926
  Mesh faces on input facets: 18926
  Mesh edges on input segments: 28383
  Steiner points on input segments:  3
  Steiner points inside domain: 5406

Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - x43A
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.0 "Blackbird"                         |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   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 2012-2022, 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: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 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: ../myMesh/tetgen_0.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 ) ----------------------
Writing solution files every 250 iterations.
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_x43a_Test.dat.
Surface file name: surface_flow_x43a_Test.
Volume file name: flow_x43a_Test.
Restart file name: restart_flow_x43a_Test.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 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.
14871 grid points.
61451 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61451 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: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525068. Standard deviation K: 2.57981.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.06744|        83.7887|
|     CV Face Area Aspect Ratio|        1.43723|        2173.76|
|           CV Sub-Volume Ratio|              1|         173135|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14871|    1/1.00|        10|
|         1|      2668|    1/5.57|   8.46005|
|         2|       485|     1/5.5|   7.18869|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597.1 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.72 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 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|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
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
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   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|  3.9254e-01|    2.731069|    5.665107|    4.728786|    8.730545|   -0.436821|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  3.8484e-01|    3.111151|    6.144144|    5.696527|    9.110995|   -0.142019|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  3.8029e-01|    3.211606|    6.272645|    5.788253|    9.178383|   -0.024212|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  3.8222e-01|    3.212276|    6.263360|    5.685266|    9.173095|    0.000170|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  3.8329e-01|    3.198810|    6.249774|    5.549315|    9.170668|   -0.026654|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.19881|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |
|CSV file                           |surface_flow_x43a_Test.csv         |
|Paraview                           |flow_x43a_Test.vtu                 |
|Paraview surface                   |surface_flow_x43a_Test.vtu         |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
Warning: there are 135 non-physical points in the solution.
Warning: 506 reconstructed states for upwinding are non-physical.

------------------------- Solver Postprocessing -------------------------
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 Force - Pressure + Viscous
Cl =  -3.127208 Cd =  117.324459
Cmx =  -34.067503 Cmy =  9269.22877 Cmz =  116.064843
Cx =  117.327335 Cy =  1.889135 Cz =  3.017366

real	0m20.838s
user	0m34.293s
sys	0m1.209s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================

./execute_PyTestRegression.sh: line 388: ulimit: stack size: cannot modify limit: Operation not permitted

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 7.674092
 Tessellating body 1 with  MaxEdge = 0.191852  Sag = 0.007674  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.13578165
C_Y  -0.0022260526
C_N  0.0034959012
C_D  0.13582094
C_S  -0.0022260526
C_L  -0.0012449398
C_l  -0.00114789
C_m  -0.00654661
C_n  0.0353227
C_M_x  8.55497e-05
C_M_y  -0.00654661
C_M_z  0.0353412

real	0m13.435s
user	0m22.980s
sys	0m0.697s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084180
 Tessellating body 1 with  MaxEdge = 0.252104  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7 -mesh2d > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:21) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (06:47:22) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
alpha [2.]  CL2 [0.11325161]  CL 0.3365288
alpha [2.]  CL2 [0.11325161]  CL 0.3365288
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:23) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (06:47:26) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:47:27) Linearizing cut-cells
   (06:47:27) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:47:27) Computing gradients
   (06:47:31) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10892098]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:32) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (06:47:37) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:47:38) Linearizing cut-cells
   (06:47:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:47:38) Computing gradients
   (06:47:42) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10892098]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            1     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.13252D-01    |proj g|=  1.08921D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:43) Running aero.csh on 2 core(s) in M0.5901A1.89108B0_DP1
   (06:47:45) aero.csh done
 o case M0.5901A1.89108B0_DP1, averaging data over 1 cycle(s)
alpha [1.89107902]  CL2 [0.1015741]  CL 0.31870681
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:46) Running aero.csh on 2 core(s) in M0.5901A1.89108B0_DP1
   (06:47:50) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:47:50) Linearizing cut-cells
   (06:47:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:47:50) Computing gradients
   (06:47:54) ... done
 o case M0.5901A1.89108B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10338203]]

At iterate    1    f=  1.01574D-01    |proj g|=  1.03382D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:55) Running aero.csh on 2 core(s) in M0.5901A-0.141883B0_DP1
   (06:47:58) aero.csh done
 o case M0.5901A-0.141883B0_DP1, averaging data over 1 cycle(s)
alpha [-0.14188302]  CL2 [0.0002398]  CL -0.01530209
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:47:59) Running aero.csh on 2 core(s) in M0.5901A-0.141883B0_DP1
   (06:48:02) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:48:02) Linearizing cut-cells
   (06:48:02) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:48:02) Computing gradients
   (06:48:07) ... done
 o case M0.5901A-0.141883B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00516383]]

At iterate    2    f=  2.39797D-04    |proj g|=  5.16383D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:07) Running aero.csh on 2 core(s) in M0.5901A-0.0451693B0_DP1
   (06:48:10) aero.csh done
 o case M0.5901A-0.0451693B0_DP1, averaging data over 1 cycle(s)
alpha [-0.04516934]  CL2 [2.02152408e-06]  CL 0.00115329
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:11) Running aero.csh on 2 core(s) in M0.5901A-0.0451693B0_DP1
   (06:48:13) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:48:14) Linearizing cut-cells
   (06:48:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:48:14) Computing gradients
   (06:48:18) ... done
 o case M0.5901A-0.0451693B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00044919]]

At iterate    3    f=  2.02152D-06    |proj g|=  4.49187D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:19) Running aero.csh on 2 core(s) in M0.5901A-0.0529089B0_DP1
   (06:48:21) aero.csh done
 o case M0.5901A-0.0529089B0_DP1, averaging data over 1 cycle(s)
alpha [-0.05290894]  CL2 [2.43246828e-08]  CL -0.00013421
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:22) Running aero.csh on 2 core(s) in M0.5901A-0.0529089B0_DP1
   (06:48:24) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:48:25) Linearizing cut-cells
   (06:48:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:48:25) Computing gradients
   (06:48:29) ... done
 o case M0.5901A-0.0529089B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[3.23721873e-05]]

At iterate    4    f=  2.43247D-08    |proj g|=  3.23722D-05
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:30) Running aero.csh on 2 core(s) in M0.5901A-0.05351B0_DP1
   (06:48:32) aero.csh done
 o case M0.5901A-0.05351B0_DP1, averaging data over 1 cycle(s)
alpha [-0.05351004]  CL2 [3.32931726e-09]  CL -0.00023438
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:33) Running aero.csh on 2 core(s) in M0.5901A-0.05351B0_DP1
   (06:48:36) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (06:48:36) Linearizing cut-cells
   (06:48:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (06:48:36) Computing gradients
   (06:48:40) ... done
 o case M0.5901A-0.05351B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[1.1501679e-07]]

At iterate    5    f=  3.32932D-09    |proj g|=  1.15017D-07

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    1      5      6      5     0     0   1.150D-07   3.329D-09
  F =   3.3293172641000006E-009

CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL            
Optimization Complete
-----------------------------------
Optimized value: [-0.05351004]

real	1m42.762s
user	0m58.210s
sys	0m10.592s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:44) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:48:51) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [1. 2.]  CL2 [0.04586976]  CL -0.214172
twist [1. 2.]  CL2 [0.04586976]  CL -0.214172
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:48:52) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:49:08) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:49:08) Linearizing cut-cells
   (06:49:10) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:49:10) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:49:14) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02640792 0.02619742]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:49:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:50:03) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:50:03) Linearizing cut-cells
   (06:50:05) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:50:05) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:50:09) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02640792 0.02619742]]
RUNNING THE L-BFGS-B CODE

           * * *

Machine precision = 2.220D-16
 N =            2     M =           10

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.58698D-02    |proj g|=  2.64079D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:50:11) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:50:19) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [0.97359208 1.97380258]  CL2 [0.04430268]  CL -0.210482
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:50:21) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:50:37) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:50:37) Linearizing cut-cells
   (06:50:39) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:50:40) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:50:44) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02595604 0.02574775]]

At iterate    1    f=  4.43027D-02    |proj g|=  2.59560D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:50:45) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:50:52) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.54327006  0.47374949]  CL2 [0.00011341]  CL 0.0106492
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:50:53) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:51:09) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:51:09) Linearizing cut-cells
   (06:51:11) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:51:11) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:51:15) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-0.00132498 -0.00131139]]

At iterate    2    f=  1.13406D-04    |proj g|=  1.32498D-03
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:51:17) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:51:23) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.46959911  0.54644784]  CL2 [9.69397412e-07]  CL -0.00098458
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:51:25) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:51:45) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:51:46) Linearizing cut-cells
   (06:51:48) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:51:48) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:51:52) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.00012252 0.00012118]]

At iterate    3    f=  9.69397D-07    |proj g|=  1.22516D-04
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:51:53) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:52:08) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.47583461  0.54029853]  CL2 [1.35059209e-09]  CL 3.675e-05
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (06:52:11) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (06:52:48) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (06:52:49) Linearizing cut-cells
   (06:52:51) ... done
   o Number of simultaneous xsensit jobs:  2
   (06:52:51) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (06:52:55) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-4.57244674e-06 -4.52300733e-06]]

At iterate    4    f=  1.35059D-09    |proj g|=  4.57245D-06

           * * *

Tit   = total number of iterations
Tnf   = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip  = number of BFGS updates skipped
Nact  = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F     = final function value

           * * *

   N    Tit     Tnf  Tnint  Skip  Nact     Projg        F
    2      4      5      4     0     0   4.572D-06   1.351D-09
  F =   1.3505920900000002E-009

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.47583461  0.54029853]

real	4m14.685s
user	4m13.358s
sys	0m10.135s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================


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

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

Fun3D
=================================================

All tests pass!


=================================================
=================================================
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Sleeping for 5 seconds due to JENKINS-32191...
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/CFD,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #158' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality QualityGate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #159'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS