Console Output

Skipping 434 KB.. Full Log
|   |___/\___//___|   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: ../aflr2/aflr2.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_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.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.
11153 grid points.
11485 volume elements.
3 surface markers.
24 boundary elements in index 0 (Marker = BC_3).
24 boundary elements in index 1 (Marker = BC_4).
399 boundary elements in index 2 (Marker = BC_5).
1013 triangles.
10472 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 1013 TRIANGLE volume elements.
There has been a re-orientation of 10424 QUADRILATERAL volume elements.
There has been a re-orientation of 447 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 1113.1.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.61256. Standard deviation K: 19.566.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.1197|             90|
|     CV Face Area Aspect Ratio|         1.0007|    2.05546e+32|
|           CV Sub-Volume Ratio|        1.00002|            inf|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2684|    1/4.16|   7.35846|
|         2|       532|    1/5.05|   4.91408|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 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|  9.2141e-02|    1.513916|    4.384882|    4.363742|    6.989443|    0.189848|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.8041e-02|    1.933195|    4.315411|    4.692800|    7.442893|    0.702555|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.8241e-02|    2.267767|    4.596557|    5.003376|    7.696498|    1.554110|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  8.9051e-02|    2.417497|    4.673412|    5.193903|    7.848297|    7.564990|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  8.8644e-02|    2.467641|    4.648647|    5.247837|    7.945567|  -20.801857|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  8.9097e-02|    2.558251|    4.773737|    5.362576|    8.081337|   -6.326538|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  8.9227e-02|    2.693027|    4.777593|    5.517728|    8.240654|   -3.360238|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  8.9351e-02|    2.804352|    4.865434|    5.634638|    8.340611|    5.845845|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  8.9214e-02|    2.882515|    4.894916|    5.731159|    8.459787|    0.958965|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  8.9034e-02|    2.892429|    5.000190|    5.749228|    8.482395|    1.689841|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|       2.89243|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 798 more values.0: Error finishing Tecplot file output.

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

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

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

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

real	0m3.692s
user	0m3.281s
sys	0m0.940s
+ status=0
+ set +x

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


=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 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: AFLR4_Mesh_Surf_0.dat ....
Finished writing TECPLOT file


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


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


Writing TECPLOT file: AFLR4_Mesh_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 - 6330
Number of surface elements - 12620
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     Darwin 19.6.0 x86_64
AFLR2    : Compile Date   06/10/22 @ 06:56PM
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 10.22.22
AFLR4    : Version Date   06/24/22 @ 02:23PM
AFLR4    : Compile OS     Darwin 19.6.0 x86_64
AFLR4    : Compile Date   06/24/22 @ 02:26PM
AFLR4    : Copyright 1994-2021, D.L. Marcum
AFLR4    : ---------------------------------------

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.21
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     0.421   seconds

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.21
EGADS    : OpenCASCADE Version 7.6.0
EGADS    : ---------------------------------------

OVERALL  : CPU Time          =     0.290   seconds
Volume mesh:
	Number of nodes = 39994
	Number of elements = 230794
	Number of triangles = 12620
	Number of quadrilatarals = 0
	Number of tetrahedrals = 218174
	Number of pyramids= 0
	Number of prisms= 0
	Number of hexahedrals= 0

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


Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wake
	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......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   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: ../aflr3/aflr3_0.su2

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

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

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

-------------------- Output Information ( Zone 0 ) ----------------------
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_su2AFLRTest.dat.
Surface file name: surface_flow_su2AFLRTest.
Volume file name: flow_su2AFLRTest.
Restart file name: restart_flow_su2AFLRTest.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_1|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                          Far-field|                               BC_4|
+-----------------------------------------------------------------------+
|                  Internal 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 ) -------------------
Three dimensional problem.
39994 grid points.
218174 volume elements.
4 surface markers.
6726 boundary elements in index 0 (Marker = BC_1).
5418 boundary elements in index 1 (Marker = BC_2).
72 boundary elements in index 2 (Marker = BC_3).
404 boundary elements in index 3 (Marker = BC_4).
218174 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08442e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4867.4. Mean K: 61.4052. Standard deviation K: 267.141.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        26.1608|        84.7934|
|     CV Face Area Aspect Ratio|         1.1798|        11987.9|
|           CV Sub-Volume Ratio|        1.07548|         337393|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     39994|    1/1.00|        10|
|         1|      6574|    1/6.08|    8.2168|
|         2|      1034|    1/6.36|   6.65311|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.039 m^2.
Area projection in the x-plane = 11.1556 m^2, y-plane = 4.97851 m^2, z-plane = 55.3964 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.582636 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_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|  1.2754e+00|   -0.071315|    2.290794|    2.031280|    5.419580|    1.973482|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  1.2597e+00|   -0.034608|    2.460325|    2.159740|    5.466392|    2.686091|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  1.2421e+00|    0.005199|    2.550359|    2.403104|    5.500990|    4.124017|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  1.2739e+00|   -0.033814|    2.582966|    2.545499|    5.450541|    6.078865|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  1.2451e+00|   -0.066944|    2.598024|    2.609093|    5.411777|    7.801446|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  1.2239e+00|   -0.068646|    2.607451|    2.631795|    5.418000|    9.026527|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  1.2088e+00|   -0.080590|    2.598574|    2.640463|    5.413304|    9.910577|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  1.2318e+00|   -0.118905|    2.549037|    2.646742|    5.370922|   10.421714|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  1.2268e+00|   -0.168636|    2.475290|    2.638087|    5.308991|   10.532379|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  1.2219e+00|   -0.225891|    2.398496|    2.604770|    5.239944|   10.317299|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     -0.225891|          < -8|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_su2AFLRTest.dat       |
+-----------------------------------------------------------------------+

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file                           |surface_flow_su2AFLRTest.csv       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview                           |flow_su2AFLRTest.vtu               |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface                   |surface_flow_su2AFLRTest.vtu       |

Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).

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

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

Total Force - Pressure + Viscous
Cl =  0.792893 Cd =  0.076851
Cmx =  -0.000311 Cmy =  -0.202024 Cmz =  9.8e-05
Cx =  0.063001 Cy =  8.7e-05 Cz =  0.794114
Pressure Contribution
Cl_p =  0.792893 Cd_p =  0.076851
Cmx_p =  -0.000311 Cmy_p =  -0.202024 Cmz_p =  9.8e-05
Cx_p =  0.063001 Cy_p =  8.7e-05 Cz_p =  0.794114
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmx_v =  0.0 Cmy_v =  0.0 Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0 Cz_v =  0.0

real	0m32.292s
user	0m30.835s
sys	0m1.077s
+ status=0
+ set +x

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

delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo

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

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

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


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

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	Warning: No boundary condition specified for capsGroup 2DSlice!
	Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.1) "


Running SU2......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   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|  6.4251e-02|   -1.163171|    1.073770|    1.341444|    4.312165|    0.062120|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  6.4483e-02|   -1.561828|    0.808636|    0.967487|    3.922716|    0.139775|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  6.3413e-02|   -1.601698|    0.943793|    1.009036|    3.876382|    0.373708|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  6.3191e-02|   -1.659374|    1.008221|    1.015635|    3.799753|    0.952935|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  6.2853e-02|   -1.663585|    1.011627|    0.956487|    3.788246|    2.344781|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  6.2457e-02|   -1.633451|    0.991734|    0.872954|    3.829708|    6.259549|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  6.2278e-02|   -1.626398|    0.990123|    0.847075|    3.843511|   26.349556|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  6.2371e-02|   -1.643439|    1.009125|    0.895796|    3.825758|  -56.104876|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  6.2511e-02|   -1.659565|    1.020774|    0.939260|    3.804303|  -24.431167|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  6.2706e-02|   -1.676757|    1.012633|    0.938320|    3.783310|  -21.456835|

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

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.67676|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_delaundoMesh.dat      |
+-----------------------------------------------------------------------+

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) ------------------------

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

real	0m3.260s
user	0m2.435s
sys	0m0.864s
+ status=0
+ set +x

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

pointwise: /Applications/Pointwise/PointwiseV18.5R1/pointwise

=================================================
+ echo 'su2_and_pointwise_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 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 '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Number of command line arguments = 2
Wed Jul 13 2022  3:27:27AM 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!
Wed Jul 13 2022  3:27:31AM EDT
Run Time: 00 Hours 00 Minutes 04 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Wed Jul 13 2022  3:27:31AM 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!
Wed Jul 13 2022  3:27:34AM EDT
Export Time: 00 Hours 00 Minutes 03 Seconds
Volume mesh:
	Number of nodes          = 16843
	Number of elements       = 98599
	Number of triangles      = 2986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 98599
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 548
	Number of elements = 1092
	Number of tris = 1092
	Number of quad = 0
Body = 2
	Number of nodes    = 556
	Number of elements = 1108
	Number of tris = 1108
	Number of quad = 0
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......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   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.
16843 grid points.
98599 volume elements.
3 surface markers.
786 boundary elements in index 0 (Marker = BC_1).
1092 boundary elements in index 1 (Marker = BC_2).
1108 boundary elements in index 2 (Marker = BC_3).
98599 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.11302e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 6570.86. Mean K: 103.512. Standard deviation K: 506.754.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|         42.667|        82.4507|
|     CV Face Area Aspect Ratio|        1.20723|        93.3104|
|           CV Sub-Volume Ratio|        1.00035|        2062.86|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     16843|    1/1.00|        10|
|         1|      2644|    1/6.37|   8.09168|
|         2|       387|    1/6.83|   6.39656|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 90.089 m^2.
Area projection in the x-plane = 8.32094 m^2, y-plane = 3.6838 m^2, z-plane = 42.3969 m^2.
Max. coordinate in the x-direction = 12.3619 m, y-direction = 7.07107 m, z-direction = 0.510646 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.368435 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_2 is NOT a single plane.
Boundary marker BC_3 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  5.1951e-01|    0.431318|    2.847144|    2.407979|    5.922214|    2.162720|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.9422e-01|    0.156042|    2.634244|    2.370361|    5.638293|    2.663044|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.8787e-01|    0.114372|    2.631966|    2.489176|    5.586483|    3.627433|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.9224e-01|    0.053009|    2.612274|    2.549130|    5.521984|    4.729599|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.8960e-01|    0.014424|    2.611922|    2.564028|    5.489762|    5.481903|

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

Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|     0.0144238|         < -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) ------------------------

Total Force - Pressure + Viscous
Cl =  0.660206 Cd =  0.120434
Cmx =  0.00478 Cmy =  -0.197025 Cmz =  0.000155
Cx =  0.108893 Cy =  0.000977 Cz =  0.662207

real	0m16.029s
user	0m12.761s
sys	0m2.047s
+ status=0
+ set +x

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


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

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


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


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

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

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  0.04661
Creating surface mesh ...
Surface mesh seconds:  0.011805
Recovering boundaries...
Boundary recovery seconds:  0.115321
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.008448
Suppressing Steiner points ...
Steiner suppression seconds:  1.7e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.014585
Refining mesh...
  4189 insertions, added 2138 points, 127097 tetrahedra in queue.
  1394 insertions, added 409 points, 130640 tetrahedra in queue.
  1859 insertions, added 449 points, 127916 tetrahedra in queue.
  2478 insertions, added 473 points, 111923 tetrahedra in queue.
  3303 insertions, added 484 points, 65315 tetrahedra in queue.
  4403 insertions, added 433 points, 571 tetrahedra in queue.
Refinement seconds:  1.28903
Smoothing vertices...
Mesh smoothing seconds:  1.03161
Improving mesh...
Mesh improvement seconds:  0.039655
Jettisoning redundant points.

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

Output seconds:  0.003921
Total running seconds:  2.56138

Statistics:

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

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

Done meshing using TetGen!
Volume mesher 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......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   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.
8039 grid points.
39668 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39668 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08934e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        1.83144|        84.8022|
|     CV Face Area Aspect Ratio|        1.55015|        7101.39|
|           CV Sub-Volume Ratio|        1.05639|         198266|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|      8039|    1/1.00|        10|
|         1|      1338|    1/6.01|   8.25105|
|         2|       214|    1/6.25|    6.7182|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        226952|             1|   m^2/s^2|        226952|
|            Velocity-X|       200.779|             1|       m/s|       200.779|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       3.50461|             1|       m/s|       3.50461|
|    Velocity Magnitude|       200.809|             1|       m/s|       200.809|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|        0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  2.7057e-01|    0.619384|    3.051344|    2.094590|    6.110279|    1.812161|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  2.8996e-01|    0.785542|    3.264371|    2.974872|    6.285549|    2.181906|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  2.9545e-01|    0.724139|    3.334285|    3.249736|    6.229534|    3.226648|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  2.8029e-01|    0.621976|    3.305627|    3.334988|    6.113861|    4.648342|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  2.7896e-01|    0.625390|    3.207240|    3.303991|    6.098630|    5.785533|

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

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

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) ------------------------

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

real	4m28.339s
user	4m2.640s
sys	0m1.105s
+ status=0
+ set +x

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


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

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


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

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

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds:  0.248122
Creating surface mesh ...
Surface mesh seconds:  0.057914
Recovering boundaries...
Warning:  6 segments are not recovered.
Boundary recovery seconds:  0.4494
Removing exterior tetrahedra ...
Exterior tets removal seconds:  0.025013
Suppressing Steiner points ...
Steiner suppression seconds:  2.2e-05
Recovering Delaunayness...
Delaunay recovery seconds:  0.053041
Refining mesh...
  12618 insertions, added 5266 points, 45 tetrahedra in queue.
Refinement seconds:  1.5238
Smoothing vertices...
Mesh smoothing seconds:  1.40311
Improving mesh...
Mesh improvement seconds:  0.082224
Jettisoning redundant points.

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

Output seconds:  0.011641
Total running seconds:  3.87098

Statistics:

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

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

Done meshing using TetGen!
Volume mesher 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......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   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.
14871 grid points.
61451 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61451 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525068. Standard deviation K: 2.57981.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        2.06744|        83.7887|
|     CV Face Area Aspect Ratio|        1.43723|        2173.76|
|           CV Sub-Volume Ratio|              1|         173135|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     14871|    1/1.00|        10|
|         1|      2668|    1/5.57|   8.46005|
|         2|       485|     1/5.5|   7.18869|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597.1 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.72 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.

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

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        916077|             1|   m^2/s^2|        916077|
|            Velocity-X|       1189.41|             1|       m/s|       1189.41|
|            Velocity-Y|             0|             1|       m/s|             0|
|            Velocity-Z|       62.3342|             1|       m/s|       62.3342|
|    Velocity Magnitude|       1191.04|             1|       m/s|       1191.04|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

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

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

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

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

Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  4.9321e-01|    2.731069|    5.665107|    4.728786|    8.730545|   -0.436821|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  4.7114e-01|    3.111151|    6.144144|    5.696527|    9.110995|   -0.142019|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  4.7030e-01|    3.211606|    6.272645|    5.788253|    9.178383|   -0.024212|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  4.6390e-01|    3.212276|    6.263360|    5.685266|    9.173095|    0.000170|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  4.4652e-01|    3.198810|    6.249774|    5.549315|    9.170668|   -0.026654|

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

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

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 135 non-physical points in the solution.
Warning: 506 reconstructed states for upwinding are non-physical.

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

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

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

real	0m27.394s
user	0m39.989s
sys	0m1.177s
+ status=0
+ set +x

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

./execute_PyTestRegression.sh: line 403: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//flowCart

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

real	0m17.105s
user	0m22.751s
sys	0m0.718s
+ status=0
+ set +x

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


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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - alpha
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084180
 Tessellating body 1 with  MaxEdge = 0.252104  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7  -mesh2d > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:19) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (03:33:21) aero.csh done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
alpha [2.]  CL2 [0.11325161]  CL 0.3365288
alpha [2.]  CL2 [0.11325161]  CL 0.3365288
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:22) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
   (03:33:25) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:33:25) Linearizing cut-cells
   (03:33:25) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:33:26) Computing gradients
   (03:33:30) ... done
 o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10892098]]
RUNNING THE L-BFGS-B CODE

           * * *

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

At X0         0 variables are exactly at the bounds

At iterate    0    f=  1.13252D-01    |proj g|=  1.08921D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:31) Running aero.csh on 2 core(s) in M0.5901A1.89108B0_DP1
   (03:33:33) aero.csh done
 o case M0.5901A1.89108B0_DP1, averaging data over 1 cycle(s)
alpha [1.89107902]  CL2 [0.1015741]  CL 0.31870681
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:34) Running aero.csh on 2 core(s) in M0.5901A1.89108B0_DP1
   (03:33:37) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:33:37) Linearizing cut-cells
   (03:33:37) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:33:37) Computing gradients
   (03:33:41) ... done
 o case M0.5901A1.89108B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10338203]]

At iterate    1    f=  1.01574D-01    |proj g|=  1.03382D-01
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:43) Running aero.csh on 2 core(s) in M0.5901A-0.141883B0_DP1
   (03:33:44) aero.csh done
 o case M0.5901A-0.141883B0_DP1, averaging data over 1 cycle(s)
alpha [-0.14188302]  CL2 [0.0002398]  CL -0.01530209
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:45) Running aero.csh on 2 core(s) in M0.5901A-0.141883B0_DP1
   (03:33:49) 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:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:33:49) Linearizing cut-cells
   (03:33:49) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:33:49) Computing gradients
   (03:33:53) ... done
 o case M0.5901A-0.141883B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00516383]]

At iterate    2    f=  2.39797D-04    |proj g|=  5.16383D-03
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:54) Running aero.csh on 2 core(s) in M0.5901A-0.0451693B0_DP1
   (03:33:56) aero.csh done
 o case M0.5901A-0.0451693B0_DP1, averaging data over 1 cycle(s)
alpha [-0.04516934]  CL2 [2.02152408e-06]  CL 0.00115329
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:33:57) Running aero.csh on 2 core(s) in M0.5901A-0.0451693B0_DP1
   (03:34:00) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:34:01) Linearizing cut-cells
   (03:34:01) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:34:01) Computing gradients
   (03:34:05) ... done
 o case M0.5901A-0.0451693B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00044919]]

At iterate    3    f=  2.02152D-06    |proj g|=  4.49187D-04
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:06) Running aero.csh on 2 core(s) in M0.5901A-0.0529089B0_DP1
   (03:34:08) aero.csh done
 o case M0.5901A-0.0529089B0_DP1, averaging data over 1 cycle(s)
alpha [-0.05290894]  CL2 [2.43246828e-08]  CL -0.00013421
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:09) Running aero.csh on 2 core(s) in M0.5901A-0.0529089B0_DP1
   (03:34:13) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:34:13) Linearizing cut-cells
   (03:34:13) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:34:13) Computing gradients
   (03:34:17) ... done
 o case M0.5901A-0.0529089B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[3.23721873e-05]]

At iterate    4    f=  2.43247D-08    |proj g|=  3.23722D-05
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:19) Running aero.csh on 2 core(s) in M0.5901A-0.05351B0_DP1
   (03:34:21) aero.csh done
 o case M0.5901A-0.05351B0_DP1, averaging data over 1 cycle(s)
alpha [-0.05351004]  CL2 [3.32931726e-09]  CL -0.00023438
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:22) Running aero.csh on 2 core(s) in M0.5901A-0.05351B0_DP1
   (03:34:26) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               2188
              Estimated cutter memory:  0.000219 GB / DV
              Estimated xsensit memory: 0.004157 GB / DV
              Available threads:        2
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (03:34:26) Linearizing cut-cells
   (03:34:26) ... done
   o Number of simultaneous xsensit jobs:  1
   (03:34:26) Computing gradients
   (03:34:30) ... done
 o case M0.5901A-0.05351B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[1.1501679e-07]]

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

           * * *

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

           * * *

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

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

real	1m38.022s
user	0m52.437s
sys	0m9.995s
+ status=0
+ set +x

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


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

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - twist
	Done getting CFD design variables
Getting CFD functional.......
	Number of design variables - 1
	Objective name - CL2
	Done getting CFD functional
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:35) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:34:42) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [1. 2.]  CL2 [0.04586976]  CL -0.214172
twist [1. 2.]  CL2 [0.04586976]  CL -0.214172
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:34:44) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:35:01) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (03:35:01) Linearizing cut-cells
   (03:35:03) ... done
   o Number of simultaneous xsensit jobs:  2
   (03:35:03) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (03:35:07) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02640792 0.02619742]]
RUNNING THE L-BFGS-B CODE

           * * *

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

At X0         0 variables are exactly at the bounds

At iterate    0    f=  4.58698D-02    |proj g|=  2.64079D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084443
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:35:09) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:35:17) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [0.97359208 1.97380258]  CL2 [0.04430268]  CL -0.210482
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:35:18) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:35:34) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (03:35:34) Linearizing cut-cells
   (03:35:36) ... done
   o Number of simultaneous xsensit jobs:  2
   (03:35:36) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (03:35:40) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02595604 0.02574775]]

At iterate    1    f=  4.43027D-02    |proj g|=  2.59560D-02
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:35:42) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:35:46) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.54327006  0.47374949]  CL2 [0.00011341]  CL 0.0106492
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:35:48) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:36:02) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (03:36:02) Linearizing cut-cells
   (03:36:04) ... done
   o Number of simultaneous xsensit jobs:  2
   (03:36:04) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (03:36:08) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-0.00132498 -0.00131139]]

At iterate    2    f=  1.13406D-04    |proj g|=  1.32498D-03
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:36:10) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:36:15) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.46959911  0.54644784]  CL2 [9.69398375e-07]  CL -0.00098458
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:36:16) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:36:31) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (03:36:31) Linearizing cut-cells
   (03:36:33) ... done
   o Number of simultaneous xsensit jobs:  2
   (03:36:33) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (03:36:37) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.00012252 0.00012118]]

At iterate    3    f=  9.69398D-07    |proj g|=  1.22516D-04
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 10.084437
 Tessellating body 1 with  MaxEdge = 0.252111  Sag = 0.010084  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9  > autoInputs.out
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:36:39) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:36:50) aero.csh done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.47583461  0.54029853]  CL2 [1.35062627e-09]  CL 3.675e-05
 CAPS Info: Building sensitivity information for: twist[1,1]
 CAPS Info: Building sensitivity information for: twist[2,1]
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (03:36:51) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
   (03:37:03) aero.csh done
              Max memory allowed:       32 GB
              Flow hexes:               21574
              Estimated cutter memory:  0.002157 GB / DV
              Estimated xsensit memory: 0.040991 GB / DV
              Available threads:        2
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (03:37:03) Linearizing cut-cells
   (03:37:05) ... done
   o Number of simultaneous xsensit jobs:  2
   (03:37:05) Computing gradients
              Adjusted OMP_NUM_THREADS to 1 for xsensit
   (03:37:09) ... done
 o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-4.57250462e-06 -4.52306459e-06]]

At iterate    4    f=  1.35063D-09    |proj g|=  4.57250D-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   4.573D-06   1.351D-09
  F =   1.3506262737000002E-009

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

real	2m38.912s
user	3m23.588s
sys	0m9.087s
+ status=0
+ set +x

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


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

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

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

All tests pass!


=================================================
=================================================
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Sleeping for 5 seconds due to JENKINS-32191...
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/CFD,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #164' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #165'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS