| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.6168e-02| -0.521485| 2.079409| 1.371893| 4.965390| 1.182869|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.6123e-02| -0.795894| 1.733901| 1.139977| 4.664635| 3.893206|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.6214e-02| -0.885699| 1.481333| 1.013745| 4.332779| 14.565626|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.6150e-02| -0.993750| 1.340252| 0.917512| 4.182929| 110.245147|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 3.6177e-02| -1.110400| 1.172200| 0.857005| 3.936064| -495.837992|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 3.5803e-02| -1.185766| 1.111335| 0.833878| 3.815560| 126.876277|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 3.5473e-02| -1.253010| 1.087204| 0.820499| 3.761995| 40.129370|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 3.5240e-02| -1.297506| 1.067370| 0.803440| 3.702559| 25.133461|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 3.5043e-02| -1.307387| 1.040693| 0.767965| 3.668428| 21.072343|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.30739| < -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 352 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_aflr2.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 = 0.650422 Cd = 0.030866
Cmz = 0.373254
Cx = 0.030866 Cy = 0.650422
Pressure Contribution
Cl_p = 0.650422 Cd_p = 0.030866
Cmz_p = 0.373254
Cx_p = 0.030866 Cy_p = 0.650422
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m9.488s
user 0m2.253s
sys 0m0.670s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_NodeDist_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Saving geometry
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
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
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 2D mesh for body 1 (of 1)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.3.0 arm64
AFLR2 : Compile Date 02/27/23 @ 04:31PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.032 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 11156 21767
AFLR2 QI : Nodes, Faces = 11155 819
AFLR2 QI : Nodes, Faces = 11155 10473
AFLR2 QI : Nodes, Faces = 11155 21765
AFLR2 QI : Nodes, Faces = 11154 811
AFLR2 QI : Nodes, Faces = 11154 10476
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 805
AFLR2 QI : Nodes, Faces = 11154 10479
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11154 911
AFLR2 QI : Nodes, Faces = 11154 10426
AFLR2 QI : Nodes, Faces = 11154 21763
AFLR2 QI : Nodes, Faces = 11153 915
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 QI : Nodes, Faces = 11153 917
AFLR2 QI : Nodes, Faces = 11153 10423
AFLR2 : CPU Time = 0.012 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
Writing TECPLOT file: pyCAPS_su2_aflr2.dat ....
Finished writing TECPLOT file
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.4.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.4.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../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.
11340 volume elements.
4 surface markers.
98 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_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 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 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 545 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
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: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 552| 1/4.89| 5.0056|
+-------------------------------------------+
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 NOT 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| 9.7925e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.056234|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.0636e-02| -0.451613| 2.192234| 1.565785| 5.066972| 0.050900|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 8.8715e-02| -0.564854| 2.070558| 1.491520| 4.949788| 0.047848|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.6772e-02| -0.725300| 1.921765| 1.389268| 4.788747| 0.077818|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.5524e-02| -0.880808| 1.824143| 1.269532| 4.633030| 0.179832|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 8.4795e-02| -1.034651| 1.757534| 1.156825| 4.476500| 0.433263|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 8.3985e-02| -1.217617| 1.704018| 1.116027| 4.283168| 1.048119|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 8.3279e-02| -1.321693| 1.644061| 1.144142| 4.127043| 2.709048|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.2939e-02| -1.268757| 1.569895| 1.157468| 4.142893| 13.756362|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.2628e-02| -1.220113| 1.498009| 1.133292| 4.191258| -6.205456|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22011| < -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 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.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 = 0.064255 Cd = -0.010355
Cmz = 0.067884
Cx = -0.010355 Cy = 0.064255
Pressure Contribution
Cl_p = 0.064255 Cd_p = -0.010355
Cmz_p = 0.067884
Cx_p = -0.010355 Cy_p = 0.064255
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m3.421s
user 0m3.073s
sys 0m0.561s
+ 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/7.4/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/7.4/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.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
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.3.0 arm64
AFLR2 : Compile Date 02/27/23 @ 04:31PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.17
AFLR4 : Version Date 03/03/23 @ 03:12PM
AFLR4 : Compile OS Darwin 22.3.0 arm64
AFLR4 : Compile Date 03/03/23 @ 04:58PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 39669
Number of elements = 228946
Number of triangles = 12444
Number of quadrilatarals = 0
Number of tetrahedrals = 216502
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 (7.4.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.4.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
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.
39669 grid points.
216502 volume elements.
4 surface markers.
6592 boundary elements in index 0 (Marker = BC_1).
5358 boundary elements in index 1 (Marker = BC_2).
74 boundary elements in index 2 (Marker = BC_3).
420 boundary elements in index 3 (Marker = BC_4).
216502 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: 2.08667e+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: 4873.1. Mean K: 61.8766. Standard deviation K: 266.962.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 18.5956| 85.8872|
| CV Face Area Aspect Ratio| 1.02281| 53453.5|
| CV Sub-Volume Ratio| 1.04044| 309194|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 39669| 1/1.00| 10|
| 1| 6563| 1/6.04| 8.23458|
| 2| 1012| 1/6.49| 6.62357|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.037 m^2.
Area projection in the x-plane = 11.142 m^2, y-plane = 4.96634 m^2, z-plane = 55.4188 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| 1.0329e+00| -0.066450| 2.295726| 2.031292| 5.424445| 1.984493|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0255e+00| -0.025581| 2.453972| 2.198996| 5.472181| 2.685278|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0181e+00| -0.005066| 2.525693| 2.417792| 5.485847| 4.101952|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0124e+00| -0.050447| 2.543075| 2.533988| 5.426116| 6.037404|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0222e+00| -0.085138| 2.544004| 2.579422| 5.385471| 7.716113|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.0232e+00| -0.103068| 2.553346| 2.593184| 5.379660| 8.907613|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.0201e+00| -0.127457| 2.548706| 2.604126| 5.367470| 9.801175|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0133e+00| -0.159674| 2.519203| 2.617065| 5.334981| 10.341086|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0138e+00| -0.186506| 2.468122| 2.618430| 5.298900| 10.457873|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0133e+00| -0.229692| 2.413753| 2.595564| 5.250064| 10.257836|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.229692| < -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 = 0.793268 Cd = 0.077333
Cmx = -0.000515 Cmy = -0.202322 Cmz = -0.00015
Cx = 0.063477 Cy = -0.000213 Cz = 0.794497
Pressure Contribution
Cl_p = 0.793268 Cd_p = 0.077333
Cmx_p = -0.000515 Cmy_p = -0.202322 Cmz_p = -0.00015
Cx_p = 0.063477 Cy_p = -0.000213 Cz_p = 0.794497
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 0m35.130s
user 0m33.961s
sys 0m0.979s
+ 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/7.4/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/7.4/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 (7.4.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.4.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
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.
6316 grid points.
12338 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).
12338 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: 10.8141. 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| 89.1863|
| CV Face Area Aspect Ratio| 1.01228| 15.7098|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6316| 1/1.00| 10|
| 1| 1836| 1/3.44| 8.08736|
| 2| 528| 1/3.48| 6.50547|
+-------------------------------------------+
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 = -0.00104577 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| 6.3466e-02| -1.163033| 1.073908| 1.341581| 4.312303| 0.061759|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 6.1232e-02| -1.559277| 0.821766| 0.974274| 3.925695| 0.143033|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 6.0083e-02| -1.597691| 0.952178| 1.026365| 3.881275| 0.384276|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.9931e-02| -1.665176| 1.000446| 1.033204| 3.794339| 0.985267|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 6.0482e-02| -1.656365| 1.003953| 0.968640| 3.797516| 2.439742|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 6.0475e-02| -1.625195| 0.993840| 0.865328| 3.839909| 6.566600|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 6.0272e-02| -1.625026| 1.001945| 0.834788| 3.848896| 28.581195|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 6.0151e-02| -1.650929| 1.022751| 0.893296| 3.825476| -52.880348|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 5.9991e-02| -1.680845| 1.030964| 0.940847| 3.791964| -24.044172|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 5.9930e-02| -1.693786| 1.018104| 0.935528| 3.772368| -21.085056|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.69379| < -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 = 0.797481 Cd = -0.037822
Cmz = 0.409843
Cx = -0.037822 Cy = 0.797481
Pressure Contribution
Cl_p = 0.797481 Cd_p = -0.037822
Cmz_p = 0.409843
Cx_p = -0.037822 Cy_p = 0.797481
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.493s
user 0m2.428s
sys 0m0.700s
+ 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/7.4/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/7.4/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/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_pointwise_PyTest.py", line 67, in <module>
pointwise.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
pointwiseAIM.c:2956 in aimPostAnalysis():
Error: Pointwise did not generate caps.GeomToMesh.ugrid or caps.GeomToMesh.lb8.ugrid!
Please make sure you are using Pointwise V18.4 or newer.
================================================================================
real 6m10.118s
user 0m6.782s
sys 0m2.131s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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/7.4/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, elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.048831
Creating surface mesh ...
Surface mesh seconds: 0.015752
Recovering boundaries...
Boundary recovery seconds: 0.124753
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.013109
Suppressing Steiner points ...
Steiner suppression seconds: 1.5e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.017605
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: 1.35522
Smoothing vertices...
Mesh smoothing seconds: 0.942999
Improving mesh...
Mesh improvement seconds: 0.040014
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005195
Total running seconds: 2.56392
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.
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 (7.4.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.4.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
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| 1.9878e-01| 0.619384| 3.051344| 2.094590| 6.110279| 1.812161|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.9773e-01| 0.785542| 3.264371| 2.974872| 6.285549| 2.181906|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.9771e-01| 0.724139| 3.334285| 3.249736| 6.229534| 3.226648|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.0891e-01| 0.621976| 3.305627| 3.334988| 6.113861| 4.648342|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.0787e-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 3m49.518s
user 3m39.977s
sys 0m1.084s
+ 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/7.4/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/7.4/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 = 3817
Number of elements = 7634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7634
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 = 9471
Total number of elements = 18938
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 - 9471, elements - 18938
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.129193
Creating surface mesh ...
Surface mesh seconds: 0.062871
Recovering boundaries...
Warning: 4 segments are not recovered.
Boundary recovery seconds: 0.343015
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.035203
Suppressing Steiner points ...
Steiner suppression seconds: 1.7e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.044834
Refining mesh...
12628 insertions, added 5236 points, 17888 tetrahedra in queue.
Refinement seconds: 1.36176
Smoothing vertices...
Mesh smoothing seconds: 1.12219
Improving mesh...
Mesh improvement seconds: 0.066008
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.010613
Total running seconds: 3.18915
Statistics:
Input points: 9471
Input facets: 18938
Input segments: 28407
Input holes: 1
Input regions: 0
Mesh points: 14886
Mesh tetrahedra: 61568
Mesh faces: 132607
Mesh faces on exterior boundary: 18942
Mesh faces on input facets: 18942
Mesh edges on input segments: 28409
Steiner points on input segments: 2
Steiner points inside domain: 5413
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
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 (7.4.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.4.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../myMesh/tetgen_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
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.
14886 grid points.
61568 volume elements.
2 surface markers.
7638 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61568 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: 0.525658. Standard deviation K: 2.58025.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 5.07174| 85.1405|
| CV Face Area Aspect Ratio| 1.45022| 4704.39|
| CV Sub-Volume Ratio| 1| 565850|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14886| 1/1.00| 10|
| 1| 2691| 1/5.53| 8.48144|
| 2| 492| 1/5.47| 7.22068|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597 m^2.
Area projection in the x-plane = 761.658 m^2, y-plane = 2062.86 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 916077| 1| m^2/s^2| 916077|
| Velocity-X| 1189.41| 1| m/s| 1189.41|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 62.3342| 1| m/s| 62.3342|
| Velocity Magnitude| 1191.04| 1| m/s| 1191.04|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.5965e-01| 2.730739| 5.664690| 4.728517| 8.730214| -0.336153|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.6434e-01| 3.140776| 6.205333| 5.699116| 9.137310| -0.076874|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.6268e-01| 3.244839| 6.325687| 5.751771| 9.212144| -0.010503|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.7056e-01| 3.245828| 6.274651| 5.623307| 9.186545| -0.025707|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.6976e-01| 3.240025| 6.292112| 5.497107| 9.220877| -0.059154|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.24003| < -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 134 non-physical points in the solution.
Warning: 73 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 = -6.942853 Cd = 117.368589
Cmx = 15.111768 Cmy = 9503.574586 Cmz = -3.485496
Cx = 117.5711 Cy = -0.867756 Cz = -0.790741
real 0m20.802s
user 0m35.170s
sys 0m1.186s
+ 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/7.4/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/7.4/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 = 3.796888
Tessellating body 1 with MaxEdge = 0.094922 Sag = 0.003797 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out
Executing: ./aero.csh > aero.out
Sat Mar 11 05:07:57 EST 2023
-rwx------ 1 jenkins 77175 Mar 11 05:07 ./aero.csh
CART3D env variable set to: /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28
CART3D_ARCH env variable set to: OSX64_ICC
Using codes:
-rwxr-xr-- 1 jenkins 1558776 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//cubes
-rwxr-xr-- 1 jenkins 1292272 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//mgPrep
-rwxr-xr-- 1 jenkins 4000008 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//flowCart
-rwxr-xr-- 1 jenkins 4374960 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//xsensit
-rwxr-xr-- 1 jenkins 4168768 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adjointCart
-rwxr-xr-- 1 jenkins 12944448 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adjointErrorEst_quad
-rwxr-xr-- 1 jenkins 2952992 Oct 27 2020 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adapt
md5 checksums:
83388126060516d9809ae90219324ec2 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//cubes
b931a45f0a6528e9e0a09dd8bbdc3112 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//mgPrep
e6b7a582f48fdfcfa826ace8e16ae775 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//flowCart
0a21c9bbb7cbe180fb260828930d5e51 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//xsensit
4700b7139293eedfe3cf9ec973695073 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adjointCart
7daf88cd4774ca932186a9814f2f180d /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adjointErrorEst_quad
34e91e2cc2f93cdcf420065832acd385 /Users/jenkins/util/cart3d/cart3d_v1.5.7_OSX64_ICC--20.10.28/bin/OSX64_ICC//adapt
Building initial mesh
ERROR: CUBES failed in /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3dTest/Scratch/cart3dAIM0/inputs/adapt00
===> ERROR: Cannot execute cubes -- please contact Cart3D developers.
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_PyTest.py", line 61, in <module>
print ("C_A " + str(myAnalysis.output.C_A))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1950, in __getattr__
return self._capsItems[name].value
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1880, in value
return self._valObj.getValue()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================
real 0m4.212s
user 0m3.673s
sys 0m0.483s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> alpha [2.]
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 = 3.625615
Tessellating body 1 with MaxEdge = 0.090640 Sag = 0.003626 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
(05:08:23) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
c3d_runAero.pl FAILED: aero.csh failed
Read OUT file in /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/Cart3D_OpenMDAO_v3_alpha/Scratch/cart3d/design/M0.5901A2B0_DP1
ERROR c3d_objGrad.csh: c3d_runAero.pl failed
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 72, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 237, in <module>
omProblem.run_driver()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/utils/hooks.py", line 131, in execute_hooks
ret = f(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/problem.py", line 686, in run_driver
return self.driver.run()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/drivers/scipy_optimizer.py", line 276, in run
model.run_solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 4678, in run_solve_nonlinear
self._solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/group.py", line 2534, in _solve_nonlinear
self._nonlinear_solver._solve_with_cache_check()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 26, in _solve_with_cache_check
self.solve() # don't use caching
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 45, in solve
self._gs_iter()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/solver.py", line 793, in _gs_iter
subsys._solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 320, in _solve_nonlinear
self._compute_wrapper()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib/python3.9/contextlib.py", line 137, in __exit__
self.gen.throw(typ, value, traceback)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2964, in _call_user_function
raise err_type(
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 72, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 'cart3dSystem' <class Cart3dAnalysis>: Error calling compute(), CAPS_EXECERR:
================================================================================
================================================================================
(undefined error)
real 0m25.736s
user 0m5.287s
sys 0m0.999s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> twist [4.]
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 = 3.630958
Tessellating body 1 with MaxEdge = 0.018155 Sag = 0.000908 Angle = 10.000000
Executing: autoInputs -r 5.123450 -nDiv 5 -maxR 7 -symmY -halfBody > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(05:08:30) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
c3d_runAero.pl FAILED: aero.csh failed
Read OUT file in /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/Cart3D_OpenMDAO_v3_twist/Scratch/cart3d/design/M0.5901A0B0_DP1
ERROR c3d_objGrad.csh: c3d_runAero.pl failed
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 73, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================
During handling of the above exception, another exception occurred:
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 257, in <module>
omProblem.run_driver()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/utils/hooks.py", line 131, in execute_hooks
ret = f(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/problem.py", line 686, in run_driver
return self.driver.run()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/drivers/scipy_optimizer.py", line 276, in run
model.run_solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 4678, in run_solve_nonlinear
self._solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/group.py", line 2534, in _solve_nonlinear
self._nonlinear_solver._solve_with_cache_check()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 26, in _solve_with_cache_check
self.solve() # don't use caching
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 45, in solve
self._gs_iter()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/solver.py", line 793, in _gs_iter
subsys._solve_nonlinear()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 320, in _solve_nonlinear
self._compute_wrapper()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.9.13/lib/python3.9/contextlib.py", line 137, in __exit__
self.gen.throw(typ, value, traceback)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2964, in _call_user_function
raise err_type(
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 73, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS error code 'cart3dSystem' <class Cart3dAnalysis>: Error calling compute(), CAPS_EXECERR:
================================================================================
================================================================================
(undefined error)
real 0m6.872s
user 0m6.869s
sys 0m0.804s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing TECPLOT file: pyCAPS_AFLR4_AFLR3.dat ....
Finished writing TECPLOT file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.3.0 arm64
AFLR2 : Compile Date 02/27/23 @ 04:31PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.17
AFLR4 : Version Date 03/03/23 @ 03:12PM
AFLR4 : Compile OS Darwin 22.3.0 arm64
AFLR4 : Compile Date 03/03/23 @ 04:58PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 81944
Number of elements = 478100
Number of triangles = 15694
Number of quadrilatarals = 0
Number of tetrahedrals = 462406
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - Alpha
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Cd2
Objective name - Const
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
real 0m14.749s
user 0m13.199s
sys 0m0.883s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case fun3d_Morph_PyTest.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
Fun3D
=================================================
=================================================
Summary of examples NOT finished as expected
su2_and_pointwise_PyTest.py
cart3d_PyTest.py
cart3d_OpenMDAO_3_alpha_PyTest.py
cart3d_OpenMDAO_3_twist_PyTest.py
See pyCAPSlog.txt for more details.
=================================================
=================================================
=================================================
++ true
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/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/7.4/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 (7.4,CAPS/CFD,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #176' 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=7.4,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #177'.
[Checks API] No suitable checks publisher found.
Build step 'Console output (build log) parsing' changed build result to FAILURE
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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