Console Output

Skipping 480 KB.. Full Log
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==2880197== Warning: invalid file descriptor 1048564 in syscall close()
==2880197== Warning: invalid file descriptor 1048565 in syscall close()
==2880197== Warning: invalid file descriptor 1048566 in syscall close()
==2880197== Warning: invalid file descriptor 1048567 in syscall close()
==2880197==    Use --log-fd=<number> to select an alternative log fd.
==2880197== Warning: invalid file descriptor 1048568 in syscall close()
==2880197== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "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 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_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 at least 2 surfaces (outlet, inlet, ...)

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
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|  8.0777e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.0187e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  7.9583e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  7.9132e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  7.8729e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  7.8570e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  7.8593e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349557|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  7.8597e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104873|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  7.8403e-02|   -1.659565|    1.020774|    0.939260|    3.804302|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  7.8281e-02|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456834|

----------------------------- 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      |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file                           |surface_flow_delaundoMesh.csv      |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary                     |flow_delaundoMesh.szplt            |

Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|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) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
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
==2880040== 
==2880040== HEAP SUMMARY:
==2880040==     in use at exit: 4,287,230 bytes in 24,709 blocks
==2880040==   total heap usage: 651,404 allocs, 626,695 frees, 384,888,993 bytes allocated
==2880040== 
==2880040== LEAK SUMMARY:
==2880040==    definitely lost: 0 bytes in 0 blocks
==2880040==    indirectly lost: 0 bytes in 0 blocks
==2880040==      possibly lost: 0 bytes in 0 blocks
==2880040==    still reachable: 0 bytes in 0 blocks
==2880040==         suppressed: 4,287,230 bytes in 24,709 blocks
==2880040== 
==2880040== For lists of detected and suppressed errors, rerun with: -s
==2880040== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1866 from 1866)
40.43user 1.14system 0:41.45elapsed 100%CPU (0avgtext+0avgdata 464444maxresident)k
0inputs+15064outputs (0major+386189minor)pagefaults 0swaps

real	0m41.455s
user	0m40.438s
sys	0m1.151s
+ status=0
+ set +x

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

pointwise: /home/jenkins/util/pointwise/PointwiseV18.5R1/pointwise

=================================================
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_pointwise_PyTest.py test;'
su2_and_pointwise_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==2880228== Memcheck, a memory error detector
==2880228== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2880228== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2880228== Command: python -u su2_and_pointwise_PyTest.py -outLevel=0
==2880228== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Number of command line arguments = 2
Tue Sep 06 2022  8:27:10AM 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 19 entries.
  Quilt quilt-1: edge tolerance = 5e-07
  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 = 6.19984e-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 = 8.32902e-05
  Quilt quilt-18: edge tolerance = 6.19601e-06
  Quilt quilt-19: 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 19 entries.
Quilt list has 19 entries.
Original connector list has 36 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 36 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 8.329e-05 on con-27
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/36, name = con-1
Checking dimension for connector 2/36, name = con-2
  Changing dimension for connector 2/36 from 10 to 3
Checking dimension for connector 3/36, name = con-3
Checking dimension for connector 4/36, name = con-4
  Changing dimension for connector 4/36 from 10 to 3
Checking dimension for connector 5/36, name = con-5
  Changing dimension for connector 5/36 from 10 to 4
Checking dimension for connector 6/36, name = con-6
Checking dimension for connector 7/36, name = con-7
  Changing dimension for connector 7/36 from 10 to 3
Checking dimension for connector 8/36, name = con-8
Checking dimension for connector 9/36, name = con-9
  Changing dimension for connector 9/36 from 10 to 3
Checking dimension for connector 10/36, name = con-10
  Changing dimension for connector 10/36 from 10 to 3
Checking dimension for connector 11/36, name = con-11
  Changing dimension for connector 11/36 from 10 to 3
Checking dimension for connector 12/36, name = con-12
Checking dimension for connector 13/36, name = con-13
  Changing dimension for connector 13/36 from 10 to 4
Checking dimension for connector 14/36, name = con-14
Checking dimension for connector 15/36, name = con-16
  Changing dimension for connector 15/36 from 10 to 3
Checking dimension for connector 16/36, name = con-17
Checking dimension for connector 17/36, name = con-20
  Changing dimension for connector 17/36 from 10 to 3
Checking dimension for connector 18/36, name = con-21
Checking dimension for connector 19/36, name = con-24
  Changing dimension for connector 19/36 from 10 to 3
Checking dimension for connector 20/36, name = con-25
  Changing dimension for connector 20/36 from 10 to 4
Checking dimension for connector 21/36, name = con-26
Checking dimension for connector 22/36, name = con-27
  Changing dimension for connector 22/36 from 10 to 3
Checking dimension for connector 23/36, name = con-28
Checking dimension for connector 24/36, name = con-29
  Changing dimension for connector 24/36 from 10 to 3
Checking dimension for connector 25/36, name = con-30
  Changing dimension for connector 25/36 from 10 to 3
Checking dimension for connector 26/36, name = con-31
  Changing dimension for connector 26/36 from 10 to 3
Checking dimension for connector 27/36, name = con-32
Checking dimension for connector 28/36, name = con-33
  Changing dimension for connector 28/36 from 10 to 4
Checking dimension for connector 29/36, name = con-34
Checking dimension for connector 30/36, name = con-36
  Changing dimension for connector 30/36 from 10 to 3
Checking dimension for connector 31/36, name = con-37
Checking dimension for connector 32/36, name = con-40
  Changing dimension for connector 32/36 from 10 to 3
Checking dimension for connector 33/36, name = con-41
Checking dimension for connector 34/36, name = con-44
  Changing dimension for connector 34/36 from 10 to 3
Checking dimension for connector 35/36, name = con-45
Checking dimension for connector 36/36, name = con-46
Processing spacing values for connector 1/36, name = con-1
Processing spacing values for connector 2/36, name = con-2
Processing spacing values for connector 3/36, name = con-3
Processing spacing values for connector 4/36, name = con-4
Processing spacing values for connector 5/36, name = con-5
Processing spacing values for connector 6/36, name = con-6
Processing spacing values for connector 7/36, name = con-7
Processing spacing values for connector 8/36, name = con-8
Processing spacing values for connector 9/36, name = con-9
Processing spacing values for connector 10/36, name = con-10
Processing spacing values for connector 11/36, name = con-11
Processing spacing values for connector 12/36, name = con-12
Processing spacing values for connector 13/36, name = con-13
Processing spacing values for connector 14/36, name = con-14
Processing spacing values for connector 15/36, name = con-16
Processing spacing values for connector 16/36, name = con-17
Processing spacing values for connector 17/36, name = con-20
Processing spacing values for connector 18/36, name = con-21
Processing spacing values for connector 19/36, name = con-24
Processing spacing values for connector 20/36, name = con-25
Processing spacing values for connector 21/36, name = con-26
Processing spacing values for connector 22/36, name = con-27
Processing spacing values for connector 23/36, name = con-28
Processing spacing values for connector 24/36, name = con-29
Processing spacing values for connector 25/36, name = con-30
Processing spacing values for connector 26/36, name = con-31
Processing spacing values for connector 27/36, name = con-32
Processing spacing values for connector 28/36, name = con-33
Processing spacing values for connector 29/36, name = con-34
Processing spacing values for connector 30/36, name = con-36
Processing spacing values for connector 31/36, name = con-37
Processing spacing values for connector 32/36, name = con-40
Processing spacing values for connector 33/36, name = con-41
Processing spacing values for connector 34/36, name = con-44
Processing spacing values for connector 35/36, name = con-45
Processing spacing values for connector 36/36, name = con-46
Number of unique endpoints = 24
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/36, con-1.
    Connector dimension changed from 10 to 15, avg. spacing changed from 1.57135 to 1.01015
  Proximity test for connector 2/36, con-2.
    Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625
  Proximity test for connector 3/36, con-3.
    Connector dimension changed from 10 to 15, avg. spacing changed from 1.57135 to 1.01015
  Proximity test for connector 4/36, con-4.
    Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625
  Proximity test for connector 5/36, con-5.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.33869 to 0.286862
  Proximity test for connector 6/36, con-6.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 7/36, con-7.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 8/36, con-8.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 9/36, con-9.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 10/36, con-10.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
  Proximity test for connector 11/36, con-11.
  Proximity test for connector 12/36, con-12.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
  Proximity test for connector 13/36, con-13.
    Connector dimension changed from 4 to 15, avg. spacing changed from 1.26705 to 0.271511
  Proximity test for connector 14/36, con-14.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 15/36, con-16.
  Proximity test for connector 16/36, con-17.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
  Proximity test for connector 17/36, con-20.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
  Proximity test for connector 18/36, con-21.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
  Proximity test for connector 19/36, con-24.
  Proximity test for connector 20/36, con-25.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.535476 to 0.114745
  Proximity test for connector 21/36, con-26.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 22/36, con-27.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 23/36, con-28.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 24/36, con-29.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 25/36, con-30.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
  Proximity test for connector 26/36, con-31.
  Proximity test for connector 27/36, con-32.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
  Proximity test for connector 28/36, con-33.
    Connector dimension changed from 4 to 15, avg. spacing changed from 0.506821 to 0.108604
  Proximity test for connector 29/36, con-34.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 30/36, con-36.
  Proximity test for connector 31/36, con-37.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
  Proximity test for connector 32/36, con-40.
    Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
  Proximity test for connector 33/36, con-41.
    Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
  Proximity test for connector 34/36, con-44.
  Proximity test for connector 35/36, con-45.
    Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
  Proximity test for connector 36/36, con-46.
    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 = 9
Connector con-3 current dim = 15
Connector con-4 current dim = 9
Connector con-5 current dim = 15
Connector con-6 current dim = 15
Connector con-7 current dim = 15
Connector con-8 current dim = 15
Connector con-9 current dim = 15
Connector con-10 current dim = 15
Connector con-11 current dim = 3
Connector con-12 current dim = 15
Connector con-13 current dim = 15
Connector con-14 current dim = 15
Connector con-16 current dim = 3
Connector con-17 current dim = 15
Connector con-20 current dim = 15
Connector con-21 current dim = 15
Connector con-24 current dim = 3
Connector con-25 current dim = 15
Connector con-26 current dim = 15
Connector con-27 current dim = 15
Connector con-28 current dim = 15
Connector con-29 current dim = 15
Connector con-30 current dim = 15
Connector con-31 current dim = 3
Connector con-32 current dim = 15
Connector con-33 current dim = 15
Connector con-34 current dim = 15
Connector con-36 current dim = 3
Connector con-37 current dim = 15
Connector con-40 current dim = 15
Connector con-41 current dim = 15
Connector con-44 current dim = 3
Connector con-45 current dim = 15
Connector con-46 current dim = 15
Domain list has 19 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 8.32902e-05
Number of periodic target domains = 0
Unstructured domain 1 of 19:
  boundary name = Wake.
Unstructured domain 2 of 19:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 3 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 4 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 5 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 6 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 7 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 8 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 10 of 19:
  boundary name = Wing2.
    Creating boundary name Wing2
Unstructured domain 11 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 12 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 13 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 14 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 15 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 16 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 17 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 18 of 19:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 19 of 19:
  boundary name = Farfield.
    Farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Number of baffles = 1
Adjusting connector dimensions and distributions for wake treatment.
Number of exit connectors = 0
Number of wake edge connectors = 4
Number of TE connectors = 0
Number of exit nodes = 0
Number of TE nodes = 0
New minimum spacing for Wake treatment = 1.0e20
  WARNING: T-Rex wall boundary con-1 not found!
  WARNING: T-Rex wall boundary con-2 not found!
  WARNING: T-Rex wall boundary con-3 not found!
  WARNING: T-Rex wall boundary con-4 not found!
Adding Edge connector con-1 to redimension list.
Adding Edge connector con-2 to redimension list.
Adding Edge connector con-3 to redimension list.
Adding Edge connector con-4 to redimension list.
Checking connector con-1
Checking connector con-2
Checking connector con-3
Checking connector con-4
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 19 entries.
Baffle domain dom-1
Number of baffles = 1
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!
Tue Sep 06 2022  8:27:15AM EDT
Run Time: 00 Hours 00 Minutes 05 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Sep 06 2022  8:27:16AM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 104 / 104 curves to EGADS originals
GMA contains 36 edge groups
GMA contains 19 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Sep 06 2022  8:27:19AM EDT
Export Time: 00 Hours 00 Minutes 03 Seconds
Volume mesh:
	Number of nodes          = 16819
	Number of elements       = 98419
	Number of triangles      = 2982
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 98419
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 547
	Number of elements = 1090
	Number of tris = 1090
	Number of quad = 0
Body = 2
	Number of nodes    = 555
	Number of elements = 1106
	Number of tris = 1106
	Number of quad = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body = 3
	Number of nodes    = 147
	Number of elements = 248
	Number of tris = 248
	Number of quad = 0
Body = 4
	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 (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='pyCAPS_SU2_Pointwise.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==2880545== Warning: invalid file descriptor 1048564 in syscall close()
==2880545== Warning: invalid file descriptor 1048565 in syscall close()
==2880545== Warning: invalid file descriptor 1048566 in syscall close()
==2880545== Warning: invalid file descriptor 1048567 in syscall close()
==2880545==    Use --log-fd=<number> to select an alternative log fd.
==2880545== Warning: invalid file descriptor 1048568 in syscall close()
==2880545== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "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 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_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 at least 2 surfaces (outlet, inlet, ...)

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
16819 grid points.
98419 volume elements.
3 surface markers.
786 boundary elements in index 0 (Marker = BC_1).
1090 boundary elements in index 1 (Marker = BC_2).
1106 boundary elements in index 2 (Marker = BC_3).
98419 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: 2.11289e+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: 103.587. Standard deviation K: 505.135.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        41.5684|        82.5001|
|     CV Face Area Aspect Ratio|        1.08857|        91.1857|
|           CV Sub-Volume Ratio|        1.00035|        2895.62|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     16819|    1/1.00|        10|
|         1|      2653|    1/6.34|    8.1047|
|         2|       388|    1/6.84|   6.40511|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 89.961 m^2.
Area projection in the x-plane = 8.28857 m^2, y-plane = 3.66354 m^2, z-plane = 42.3644 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|  6.4816e-01|    0.436750|    2.853995|    2.400063|    5.927645|    2.231757|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  6.5373e-01|    0.177285|    2.645328|    2.372153|    5.661650|    2.669890|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  6.5201e-01|    0.125711|    2.634560|    2.483280|    5.597319|    3.570026|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  6.6889e-01|    0.055880|    2.617338|    2.536534|    5.523303|    4.628614|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  6.5747e-01|   -0.013557|    2.609782|    2.543487|    5.459924|    5.440069|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|    -0.0135572|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Pointwise.dat|
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Pointwise.csv|

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|Tecplot binary                     |flow_pyCAPS_SU2_Pointwise.szplt    |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
|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) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.630701 Cd =  0.115936
Cmx =  0.00241 Cmy =  -0.186524 Cmz =  -0.000327
Cx =  0.104911 Cy =  -0.0007 Cz =  0.632629
==2880228== 
==2880228== HEAP SUMMARY:
==2880228==     in use at exit: 4,309,504 bytes in 24,766 blocks
==2880228==   total heap usage: 736,278 allocs, 711,512 frees, 536,971,853 bytes allocated
==2880228== 
==2880228== LEAK SUMMARY:
==2880228==    definitely lost: 0 bytes in 0 blocks
==2880228==    indirectly lost: 0 bytes in 0 blocks
==2880228==      possibly lost: 0 bytes in 0 blocks
==2880228==    still reachable: 0 bytes in 0 blocks
==2880228==         suppressed: 4,309,504 bytes in 24,766 blocks
==2880228== 
==2880228== For lists of detected and suppressed errors, rerun with: -s
==2880228== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1843 from 1843)
63.09user 2.83system 1:00.84elapsed 108%CPU (0avgtext+0avgdata 323792maxresident)k
792inputs+41704outputs (0major+447643minor)pagefaults 0swaps

real	1m0.843s
user	1m3.095s
sys	0m2.856s
+ 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 /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_Tetgen_PyTest.py -outLevel=0
==2889554== Memcheck, a memory error detector
==2889554== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2889554== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2889554== Command: python -u su2_and_Tetgen_PyTest.py -outLevel=0
==2889554== 
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:  0.659232
Creating surface mesh ...
Surface mesh seconds:  0.122998
Recovering boundaries...
Boundary recovery seconds:  2.11298
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.06884
Suppressing Steiner points ...
Steiner suppression seconds:  0.000422
Recovering Delaunayness...
Delaunay recovery seconds:  0.295473
Refining mesh...
  4188 insertions, added 2100 points, 134662 tetrahedra in queue.
  1394 insertions, added 425 points, 138812 tetrahedra in queue.
  1858 insertions, added 471 points, 136161 tetrahedra in queue.
  2477 insertions, added 507 points, 118959 tetrahedra in queue.
  3302 insertions, added 481 points, 64039 tetrahedra in queue.
  4401 insertions, added 394 points, 1342 tetrahedra in queue.
Refinement seconds:  16.6835
Smoothing vertices...
Mesh smoothing seconds:  11.6889
Improving mesh...
Mesh improvement seconds:  0.367604
Jettisoning redundant points.

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

Output seconds:  0.029828
Total running seconds:  32.0584

Statistics:

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

  Mesh points: 8009
  Mesh tetrahedra: 39254
  Mesh faces: 81642
  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: 4869

Done meshing using TetGen!
Volume mesher did not preserve 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 (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='pyCAPS_SU2_Tetgen.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==2899973== Warning: invalid file descriptor 1048564 in syscall close()
==2899973== Warning: invalid file descriptor 1048565 in syscall close()
==2899973== Warning: invalid file descriptor 1048566 in syscall close()
==2899973== Warning: invalid file descriptor 1048567 in syscall close()
==2899973==    Use --log-fd=<number> to select an alternative log fd.
==2899973== Warning: invalid file descriptor 1048568 in syscall close()
==2899973== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "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 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_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 at least 2 surfaces (outlet, inlet, ...)

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8009 grid points.
39254 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).
39254 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: 2.09074e+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.)|        2.05157|        83.9276|
|     CV Face Area Aspect Ratio|        1.31853|        36832.6|
|           CV Sub-Volume Ratio|         1.0328|    1.76867e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8009|    1/1.00|        10|
|         1|      1339|    1/5.98|    8.2634|
|         2|       221|    1/6.06|   6.79914|
+-------------------------------------------+
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|  2.7926e-01|    0.620196|    3.052156|    2.095402|    6.111091|    1.821394|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.7415e-01|    0.861155|    3.388133|    3.046216|    6.371496|    2.187054|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.7294e-01|    0.750173|    3.392367|    3.289072|    6.260635|    3.214764|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.7045e-01|    0.570309|    3.263082|    3.330629|    6.049566|    4.586176|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.7122e-01|    0.568946|    3.182696|    3.257588|    6.036569|    5.762812|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      0.568946|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_SU2_Tetgen.dat |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file                           |surface_flow_pyCAPS_SU2_Tetgen.csv |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview                           |flow_pyCAPS_SU2_Tetgen.vtu         |

Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|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) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  0.75489 Cd =  0.130993
Cmx =  -0.007921 Cmy =  -0.211909 Cmz =  0.002289
Cx =  0.117799 Cy =  0.001444 Cz =  0.757061
==2889554== 
==2889554== HEAP SUMMARY:
==2889554==     in use at exit: 4,288,829 bytes in 24,711 blocks
==2889554==   total heap usage: 945,016 allocs, 920,305 frees, 635,859,451 bytes allocated
==2889554== 
==2889554== LEAK SUMMARY:
==2889554==    definitely lost: 0 bytes in 0 blocks
==2889554==    indirectly lost: 0 bytes in 0 blocks
==2889554==      possibly lost: 0 bytes in 0 blocks
==2889554==    still reachable: 0 bytes in 0 blocks
==2889554==         suppressed: 4,288,829 bytes in 24,711 blocks
==2889554== 
==2889554== For lists of detected and suppressed errors, rerun with: -s
==2889554== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1866 from 1866)
111.55user 1.46system 1:52.95elapsed 100%CPU (0avgtext+0avgdata 366364maxresident)k
0inputs+24000outputs (0major+518840minor)pagefaults 0swaps

real	1m52.960s
user	1m51.560s
sys	0m1.470s
+ 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 /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==2900034== Memcheck, a memory error detector
==2900034== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2900034== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2900034== Command: python -u su2_X43a_PyTest.py -outLevel=0
==2900034== 
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    = 5653
Number of elements = 11302
Number of node elements          = 0
Number of line elements          = 0
Number of triangle elements      = 11302
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9461
Total number of elements = 18918

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 - 9461
Number of surface elements - 18918
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  1.62795
Creating surface mesh ...
Surface mesh seconds:  0.369848
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  5.0828
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.124053
Suppressing Steiner points ...
Steiner suppression seconds:  0.000244
Recovering Delaunayness...
Delaunay recovery seconds:  0.752478
Refining mesh...
  12616 insertions, added 5170 points, 18149 tetrahedra in queue.
Refinement seconds:  13.9603
Smoothing vertices...
Mesh smoothing seconds:  12.2224
Improving mesh...
Mesh improvement seconds:  0.572806
Jettisoning redundant points.

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

Output seconds:  0.063518
Total running seconds:  34.9423

Statistics:

  Input points: 9461
  Input facets: 18918
  Input segments: 28377
  Input holes: 1
  Input regions: 0

  Mesh points: 14832
  Mesh tetrahedra: 61120
  Mesh faces: 131702
  Mesh faces on exterior boundary: 18924
  Mesh faces on input facets: 18924
  Mesh edges on input segments: 28380
  Steiner points on input segments:  3
  Steiner points inside domain: 5368

Done meshing using TetGen!
Volume mesher did not preserve 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 (7.3.1) "


Running SU2......
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='x43a_Test.cfg' mode='r' encoding='UTF-8'>
  konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
  for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==2902691== Warning: invalid file descriptor 1048564 in syscall close()
==2902691== Warning: invalid file descriptor 1048565 in syscall close()
==2902691== Warning: invalid file descriptor 1048566 in syscall close()
==2902691== Warning: invalid file descriptor 1048567 in syscall close()
==2902691==    Use --log-fd=<number> to select an alternative log fd.
==2902691== Warning: invalid file descriptor 1048568 in syscall close()
==2902691== Warning: invalid file descriptor 1048569 in syscall close()

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 7.3.1 "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 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                 PARAVIEW|       250|
|         SURFACE_PARAVIEW|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_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 at least 2 surfaces (outlet, inlet, ...)

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

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14832 grid points.
61120 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11302 boundary elements in index 1 (Marker = BC_2).
61120 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: 0.525189. Standard deviation K: 2.58.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.85426|        83.9017|
|     CV Face Area Aspect Ratio|        1.82697|        18175.5|
|           CV Sub-Volume Ratio|              1|    2.40648e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14832|    1/1.00|        10|
|         1|      2681|    1/5.53|   8.48119|
|         2|       491|    1/5.46|   7.22453|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.7 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.48 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|  5.4878e-01|    2.731643|    5.665683|    4.729371|    8.731119|   -0.364357|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  5.4076e-01|    3.080507|    6.130761|    5.704829|    9.099189|   -0.114402|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  5.2102e-01|    3.238998|    6.327615|    5.859548|    9.209446|   -0.043482|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  5.1571e-01|    3.256395|    6.327390|    5.786152|    9.234758|   -0.032063|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  5.1441e-01|    3.162813|    6.212532|    5.616824|    9.137964|   -0.051711|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       3.16281|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_x43a_Test.dat         |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|CSV file                           |surface_flow_x43a_Test.csv         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview                           |flow_x43a_Test.vtu                 |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
|Paraview surface                   |surface_flow_x43a_Test.vtu         |

Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
Warning: there are 124 non-physical points in the solution.
Warning: 597 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) ------------------------

/home/jenkins/util/SU2/SU2-v7.3.1/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
  run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl =  -5.932185 Cd =  114.717353
Cmx =  38.748728 Cmy =  9154.23677 Cmz =  207.157404
Cx =  114.870603 Cy =  0.839477 Cz =  0.079788
==2900034== 
==2900034== HEAP SUMMARY:
==2900034==     in use at exit: 4,287,283 bytes in 24,707 blocks
==2900034==   total heap usage: 5,854,918 allocs, 5,830,211 frees, 4,882,064,532 bytes allocated
==2900034== 
==2900034== LEAK SUMMARY:
==2900034==    definitely lost: 0 bytes in 0 blocks
==2900034==    indirectly lost: 0 bytes in 0 blocks
==2900034==      possibly lost: 0 bytes in 0 blocks
==2900034==    still reachable: 0 bytes in 0 blocks
==2900034==         suppressed: 4,287,283 bytes in 24,707 blocks
==2900034== 
==2900034== For lists of detected and suppressed errors, rerun with: -s
==2900034== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1866 from 1866)
408.40user 6.23system 6:50.58elapsed 100%CPU (0avgtext+0avgdata 576008maxresident)k
0inputs+35904outputs (0major+1942299minor)pagefaults 0swaps

real	6m50.589s
user	6m48.418s
sys	0m6.232s
+ status=0
+ set +x

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

flowCart: /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//flowCart

=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_PyTest.py -outLevel=0
==2902729== Memcheck, a memory error detector
==2902729== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2902729== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2902729== Command: python -u cart3d_PyTest.py -outLevel=0
==2902729== 
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  0.13545895
C_Y  -0.0023190349
C_N  0.0017662912
C_D  0.13543807
C_S  -0.0023190349
C_L  -0.002962234
C_l  -0.00170699
C_m  -0.00604561
C_n  0.0354751
C_M_x  -0.00046789
C_M_y  -0.00604561
C_M_z  0.0355131
==2902729== 
==2902729== HEAP SUMMARY:
==2902729==     in use at exit: 4,059,837 bytes in 24,318 blocks
==2902729==   total heap usage: 532,823 allocs, 508,505 frees, 466,709,924 bytes allocated
==2902729== 
==2902729== LEAK SUMMARY:
==2902729==    definitely lost: 0 bytes in 0 blocks
==2902729==    indirectly lost: 0 bytes in 0 blocks
==2902729==      possibly lost: 0 bytes in 0 blocks
==2902729==    still reachable: 0 bytes in 0 blocks
==2902729==         suppressed: 4,059,837 bytes in 24,318 blocks
==2902729== 
==2902729== For lists of detected and suppressed errors, rerun with: -s
==2902729== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1838 from 1838)
57.31user 1.36system 0:37.34elapsed 157%CPU (0avgtext+0avgdata 297324maxresident)k
0inputs+17600outputs (0major+327023minor)pagefaults 0swaps

real	0m37.344s
user	0m57.311s
sys	0m1.369s
+ 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 /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==2902989== Memcheck, a memory error detector
==2902989== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2902989== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2902989== Command: python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
==2902989== 
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/exec_comp.py:7: DeprecationWarning: `np.complex` is a deprecated alias for the builtin `complex`. To silence this warning, use `complex` by itself. Doing this will not modify any behavior and is safe. If you specifically wanted the numpy scalar type, use `np.complex128` here.
Deprecated in NumPy 1.20; for more details and guidance: https://numpy.org/devdocs/release/1.20.0-notes.html#deprecations
  from numpy import ndarray, imag, complex as npcomplex
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning: 

  `numpy.distutils` is deprecated since NumPy 1.23.0, as a result
  of the deprecation of `distutils` itself. It will be removed for
  Python >= 3.12. For older Python versions it will remain present.
  It is recommended to use `setuptools < 60.0` for those Python versions.
  For more details, see:
    https://numpy.org/devdocs/reference/distutils_status_migration.html 


  import numpy.distutils
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/surrogate_models/response_surface.py:7: DeprecationWarning: The module numpy.dual is deprecated.  Instead of using dual, use the functions directly from numpy or scipy.
  from numpy.dual import lstsq
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/pyDOE2/doe_factorial.py:16: DeprecationWarning: the imp module is deprecated in favour of importlib; see the module's documentation for alternative uses
  import imp
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
   (08:40:05) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
   (08:40:07) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
alpha [2.]  CL2 [0.1057817]  CL 0.3252412
alpha [2.]  CL2 [0.1057817]  CL 0.3252412
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:09) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
   (08:40:12) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:40:12) Linearizing cut-cells
   (08:40:12) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:40:12) Computing gradients
   (08:40:16) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10602001]]
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=  1.05782D-01    |proj g|=  1.06020D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:18) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
   (08:40:20) aero.csh done
 o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
alpha [1.89397999]  CL2 [0.09478706]  CL 0.30787504
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:22) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
   (08:40:24) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:40:25) Linearizing cut-cells
   (08:40:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:40:25) Computing gradients
   (08:40:29) ... done
 o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10074813]]

At iterate    1    f=  9.47871D-02    |proj g|=  1.00748D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:31) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
   (08:40:33) aero.csh done
 o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
alpha [-0.13211104]  CL2 [0.00047434]  CL -0.02139385
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:35) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
   (08:40:37) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:40:37) Linearizing cut-cells
   (08:40:37) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:40:37) Computing gradients
   (08:40:41) ... done
 o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00732582]]

At iterate    2    f=  4.74339D-04    |proj g|=  7.32582D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:43) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
   (08:40:45) aero.csh done
 o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
alpha [0.00522812]  CL2 [1.32465164e-05]  CL 0.00361761
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:47) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
   (08:40:49) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:40:49) Linearizing cut-cells
   (08:40:49) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:40:50) Computing gradients
   (08:40:54) ... done
 o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.001238]]

At iterate    3    f=  1.32465D-05    |proj g|=  1.23800D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:56) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
   (08:40:57) aero.csh done
 o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01462583]  CL2 [2.89471283e-05]  CL -0.00546528
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:40:59) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
   (08:41:02) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:41:02) Linearizing cut-cells
   (08:41:02) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:41:02) Computing gradients
   (08:41:06) ... done
 o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00180066]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:08) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
   (08:41:10) aero.csh done
 o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
alpha [0.00067128]  CL2 [8.15511616e-06]  CL 0.00278569
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:12) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
   (08:41:14) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:41:14) Linearizing cut-cells
   (08:41:14) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:41:14) Computing gradients
   (08:41:18) ... done
 o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00097886]]

At iterate    4    f=  8.15512D-06    |proj g|=  9.78864D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:20) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
   (08:41:22) aero.csh done
 o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01654192]  CL2 [3.33627463e-05]  CL -0.00584049
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:24) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
   (08:41:26) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:41:26) Linearizing cut-cells
   (08:41:26) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:41:26) Computing gradients
   (08:41:30) ... done
 o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00193604]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:32) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
   (08:41:34) aero.csh done
 o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00140463]  CL2 [6.12816493e-06]  CL 0.00237962
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:36) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
   (08:41:38) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:41:38) Linearizing cut-cells
   (08:41:38) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:41:38) Computing gradients
   (08:41:42) ... done
 o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00084715]]

At iterate    5    f=  6.12816D-06    |proj g|=  8.47152D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:45) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
   (08:41:46) aero.csh done
 o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01475651]  CL2 [2.9240213e-05]  CL -0.00549114
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:48) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
   (08:41:50) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:41:51) Linearizing cut-cells
   (08:41:51) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:41:51) Computing gradients
   (08:41:55) ... done
 o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00181002]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:41:57) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
   (08:41:59) aero.csh done
 o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00259716]  CL2 [5.08191983e-06]  CL 0.002137
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:01) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
   (08:42:03) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:42:03) Linearizing cut-cells
   (08:42:03) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:42:03) Computing gradients
   (08:42:07) ... done
 o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00077084]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:09) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
   (08:42:11) aero.csh done
 o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00367151]  CL2 [4.27119297e-06]  CL 0.00192854
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:13) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
   (08:42:15) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:42:15) Linearizing cut-cells
   (08:42:15) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:42:15) Computing gradients
   (08:42:19) ... done
 o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00070603]]

At iterate    6    f=  4.27119D-06    |proj g|=  7.06030D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:22) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
   (08:42:23) aero.csh done
 o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01501269]  CL2 [2.98325477e-05]  CL -0.00554238
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:26) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
   (08:42:28) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:42:28) Linearizing cut-cells
   (08:42:28) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:42:28) Computing gradients
   (08:42:32) ... done
 o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00182884]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:34) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
   (08:42:36) aero.csh done
 o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00433344]  CL2 [3.77191769e-06]  CL 0.00179209
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:38) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
   (08:42:40) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:42:40) Linearizing cut-cells
   (08:42:40) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:42:41) Computing gradients
   (08:42:45) ... done
 o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00066572]]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:47) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
   (08:42:49) aero.csh done
 o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
alpha [-0.004888]  CL2 [3.36327638e-06]  CL 0.00167372
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (08:42:51) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
   (08:42:53) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (08:42:53) Linearizing cut-cells
   (08:42:53) ... done
   o Number of simultaneous xsensit jobs:  1
   (08:42:53) Computing gradients
   (08:42:58) ... done
 o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00062781]]

At iterate    7    f=  3.36328D-06    |proj g|=  6.27809D-04

           * * *

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      7     14      7     0     0   6.278D-04   3.363D-06
  F =   3.3632763807999997E-006

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized value: [-0.004888]
==2902989== 
==2902989== HEAP SUMMARY:
==2902989==     in use at exit: 6,476,402 bytes in 39,437 blocks
==2902989==   total heap usage: 7,320,326 allocs, 7,280,889 frees, 7,374,816,991 bytes allocated
==2902989== 
==2902989== LEAK SUMMARY:
==2902989==    definitely lost: 0 bytes in 0 blocks
==2902989==    indirectly lost: 0 bytes in 0 blocks
==2902989==      possibly lost: 0 bytes in 0 blocks
==2902989==    still reachable: 0 bytes in 0 blocks
==2902989==                       of which reachable via heuristic:
==2902989==                         stdstring          : 38 bytes in 1 blocks
==2902989==         suppressed: 6,476,402 bytes in 39,437 blocks
==2902989== 
==2902989== For lists of detected and suppressed errors, rerun with: -s
==2902989== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4562 from 4562)
380.11user 23.21system 6:08.17elapsed 109%CPU (0avgtext+0avgdata 578688maxresident)k
0inputs+171288outputs (0major+4036021minor)pagefaults 0swaps

real	6m8.182s
user	6m20.122s
sys	0m23.239s
+ 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 /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==2919973== Memcheck, a memory error detector
==2919973== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2919973== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2919973== Command: python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
==2919973== 
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/exec_comp.py:7: DeprecationWarning: `np.complex` is a deprecated alias for the builtin `complex`. To silence this warning, use `complex` by itself. Doing this will not modify any behavior and is safe. If you specifically wanted the numpy scalar type, use `np.complex128` here.
Deprecated in NumPy 1.20; for more details and guidance: https://numpy.org/devdocs/release/1.20.0-notes.html#deprecations
  from numpy import ndarray, imag, complex as npcomplex
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning: 

  `numpy.distutils` is deprecated since NumPy 1.23.0, as a result
  of the deprecation of `distutils` itself. It will be removed for
  Python >= 3.12. For older Python versions it will remain present.
  It is recommended to use `setuptools < 60.0` for those Python versions.
  For more details, see:
    https://numpy.org/devdocs/reference/distutils_status_migration.html 


  import numpy.distutils
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/openmdao/surrogate_models/response_surface.py:7: DeprecationWarning: The module numpy.dual is deprecated.  Instead of using dual, use the functions directly from numpy or scipy.
  from numpy.dual import lstsq
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP_venv/lib/python3.9/site-packages/pyDOE2/doe_factorial.py:16: DeprecationWarning: the imp module is deprecated in favour of importlib; see the module's documentation for alternative uses
  import imp
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
   (08:45:50) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:45:57) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [1. 2.]  CL2 [0.04745667]  CL -0.217845
twist [1. 2.]  CL2 [0.04745667]  CL -0.217845
 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
   (08:46:06) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:46:16) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (08:46:16) Linearizing cut-cells
   (08:46:18) ... done
   o Number of simultaneous xsensit jobs:  2
   (08:46:18) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (08:46:22) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02768712 0.02710382]]
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=  4.74567D-02    |proj g|=  2.76871D-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
   (08:46:29) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:46:36) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [0.97231288 1.97289618]  CL2 [0.04578804]  CL -0.213981
 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
   (08:46:44) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:46:53) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (08:46:53) Linearizing cut-cells
   (08:46:55) ... done
   o Number of simultaneous xsensit jobs:  2
   (08:46:55) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (08:47:00) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02718156 0.02662519]]

At iterate    1    f=  4.57880D-02    |proj g|=  2.71816D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 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
   (08:47:06) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:47:13) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.51633276  0.46520886]  CL2 [2.22501296e-05]  CL 0.004717
 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
   (08:47:20) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:47:29) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (08:47:30) Linearizing cut-cells
   (08:47:32) ... done
   o Number of simultaneous xsensit jobs:  2
   (08:47:32) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (08:47:36) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-0.00061003 -0.00059319]]

At iterate    2    f=  2.22501D-05    |proj g|=  6.10027D-04
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 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
   (08:47:42) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:47:48) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48365697  0.49806697]  CL2 [5.12328527e-08]  CL -0.00022635
 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
   (08:47:56) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:48:05) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (08:48:06) Linearizing cut-cells
   (08:48:08) ... done
   o Number of simultaneous xsensit jobs:  2
   (08:48:08) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (08:48:12) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[2.92787388e-05 2.84954539e-05]]

At iterate    3    f=  5.12329D-08    |proj g|=  2.92787D-05
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084427
 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
   (08:48:18) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:48:25) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48515345  0.49656089]  CL2 [1.32279047e-09]  CL -3.637e-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
   (08:48:32) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
   (08:48:42) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (08:48:42) Linearizing cut-cells
   (08:48:44) ... done
   o Number of simultaneous xsensit jobs:  2
   (08:48:44) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (08:48:48) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[4.70512143e-06 4.57920688e-06]]

At iterate    4    f=  1.32279D-09    |proj g|=  4.70512D-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   4.705D-06   1.323D-09
  F =   1.3227904707000001E-009

CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH             
Optimization Complete
-----------------------------------
Optimized values: [-0.48515345  0.49656089]
==2919973== 
==2919973== HEAP SUMMARY:
==2919973==     in use at exit: 6,475,797 bytes in 39,438 blocks
==2919973==   total heap usage: 6,062,011 allocs, 6,022,573 frees, 6,663,881,451 bytes allocated
==2919973== 
==2919973== LEAK SUMMARY:
==2919973==    definitely lost: 0 bytes in 0 blocks
==2919973==    indirectly lost: 0 bytes in 0 blocks
==2919973==      possibly lost: 0 bytes in 0 blocks
==2919973==    still reachable: 0 bytes in 0 blocks
==2919973==                       of which reachable via heuristic:
==2919973==                         stdstring          : 38 bytes in 1 blocks
==2919973==         suppressed: 6,475,797 bytes in 39,438 blocks
==2919973== 
==2919973== For lists of detected and suppressed errors, rerun with: -s
==2919973== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4584 from 4584)
524.89user 14.20system 5:51.01elapsed 153%CPU (0avgtext+0avgdata 579560maxresident)k
0inputs+144416outputs (0major+3039297minor)pagefaults 0swaps

real	5m51.017s
user	8m44.898s
sys	0m14.226s
+ status=0
+ set +x

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


=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==2928290== Memcheck, a memory error detector
==2928290== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==2928290== Using Valgrind-3.17.0 and LibVEX; rerun with -h for copyright info
==2928290== Command: python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
==2928290== 
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_0.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_1.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_2.dat ....
Finished writing TECPLOT file


Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_Surf_3.dat ....
Finished writing TECPLOT file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Number of surface nodes - 7964
Number of surface elements - 15886
Getting volume mesh
 
AFLR2    : ---------------------------------------
AFLR2    : AFLR2 LIBRARY
AFLR2    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2    : TRIA/QUAD GRID GENERATOR
AFLR2    : Version Number 9.14.3
AFLR2    : Version Date   06/09/22 @ 05:16PM
AFLR2    : Compile OS     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2    : Compile Date   06/13/22 @ 12:42PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR4    : ---------------------------------------
AFLR4    : AFLR4 LIBRARY
AFLR4    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4    : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4    : Version Number 10.22.23
AFLR4    : Version Date   07/14/22 @ 02:23PM
AFLR4    : Compile OS     Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4    : Compile Date   07/19/22 @ 12:23AM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     7.178   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.22
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     5.651   seconds
Volume mesh:
	Number of nodes = 56556
	Number of elements = 327681
	Number of triangles = 15886
	Number of quadrilatarals = 0
	Number of tetrahedrals = 311795
	Number of pyramids= 0
	Number of prisms= 0
	Number of hexahedrals= 0

Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Warning: No boundary condition specified for capsGroup Wake!
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - Alpha
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 2
	Objective name - Cd2
	Objective name - Const
	Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
 CAPS Info: Building sensitivity information for: twist[1,1]
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing sensitivity file for body 4, File - Rubberize/model.tec.4.sd1
Writing rubber.data 

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
Projecting tessellation 1 (of 4) on to new body
Projecting tessellation 2 (of 4) on to new body
Projecting tessellation 3 (of 4) on to new body
Projecting tessellation 4 (of 4) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
 CAPS Info: Building sensitivity information for: twist[1,1]
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing sensitivity file for body 4, File - Rubberize/model.tec.4.sd1

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data 
==2928290== 
==2928290== HEAP SUMMARY:
==2928290==     in use at exit: 4,085,903 bytes in 24,387 blocks
==2928290==   total heap usage: 1,863,413 allocs, 1,839,026 frees, 1,813,679,633 bytes allocated
==2928290== 
==2928290== LEAK SUMMARY:
==2928290==    definitely lost: 0 bytes in 0 blocks
==2928290==    indirectly lost: 0 bytes in 0 blocks
==2928290==      possibly lost: 0 bytes in 0 blocks
==2928290==    still reachable: 0 bytes in 0 blocks
==2928290==         suppressed: 4,085,903 bytes in 24,387 blocks
==2928290== 
==2928290== For lists of detected and suppressed errors, rerun with: -s
==2928290== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1832 from 1832)
282.18user 1.71system 4:43.90elapsed 100%CPU (0avgtext+0avgdata 404152maxresident)k
0inputs+82504outputs (0major+848456minor)pagefaults 0swaps

real	4m43.907s
user	4m42.190s
sys	0m1.726s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================


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

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

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

All tests pass!

+ exit 0
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[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: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[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,LINUX64,reynolds)
[Static Analysis] Using reference build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #187' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #188'.
[Checks API] No suitable checks publisher found.
[Valgrind] Files to copy:
[Valgrind] Analysing valgrind results
[Valgrind] Ending the valgrind analysis.
[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