| 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| 4.4565e-02| -0.385358| 2.453598| 1.625650| 5.369499| 0.360386|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.5246e-02| -0.521485| 2.079409| 1.371893| 4.965390| 1.182869|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 5.3859e-02| -0.795894| 1.733901| 1.139977| 4.664635| 3.893206|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 5.8238e-02| -0.885699| 1.481333| 1.013745| 4.332779| 14.565626|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 6.0768e-02| -0.993750| 1.340252| 0.917512| 4.182929| 110.245147|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 6.2561e-02| -1.110400| 1.172200| 0.857005| 3.936064| -495.837992|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 6.4064e-02| -1.185766| 1.111335| 0.833878| 3.815560| 126.876277|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 6.6101e-02| -1.253010| 1.087204| 0.820499| 3.761995| 40.129370|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 6.7523e-02| -1.297506| 1.067370| 0.803440| 3.702559| 25.133461|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 6.8678e-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 0m3.051s
user 0m2.554s
sys 0m0.642s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2 : Compile Date 02/08/23 @ 12:48PM
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 = 0.003 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 = 0.060 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 = 0.025 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| 1.7026e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.056234|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.6698e-01| -0.451613| 2.192234| 1.565785| 5.066972| 0.050900|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.6588e-01| -0.564854| 2.070558| 1.491520| 4.949788| 0.047848|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.6234e-01| -0.725300| 1.921765| 1.389268| 4.788747| 0.077818|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.5684e-01| -0.880808| 1.824143| 1.269532| 4.633030| 0.179832|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.4846e-01| -1.034651| 1.757534| 1.156825| 4.476500| 0.433263|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.4375e-01| -1.217617| 1.704018| 1.116027| 4.283168| 1.048119|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.4227e-01| -1.321693| 1.644061| 1.144142| 4.127043| 2.709048|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.3786e-01| -1.268757| 1.569895| 1.157468| 4.142893| 13.756362|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.3860e-01| -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 0m5.158s
user 0m4.331s
sys 0m0.472s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
su2_and_AFLR4_AFLR3_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
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 Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2 : Compile Date 02/08/23 @ 12:48PM
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 Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4 : Compile Date 03/03/23 @ 11:35PM
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 = 40023
Number of elements = 231175
Number of triangles = 12446
Number of quadrilatarals = 0
Number of tetrahedrals = 218729
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.
40023 grid points.
218729 volume elements.
4 surface markers.
6594 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).
218729 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: 61.8669. Standard deviation K: 266.942.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 26.7183| 86.0113|
| CV Face Area Aspect Ratio| 1.107| 19535.2|
| CV Sub-Volume Ratio| 1.03852| 271857|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 40023| 1/1.00| 10|
| 1| 6611| 1/6.05| 8.2302|
| 2| 1024| 1/6.46| 6.62999|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.036 m^2.
Area projection in the x-plane = 11.1425 m^2, y-plane = 4.96698 m^2, z-plane = 55.4178 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| 2.1744e+00| -0.068489| 2.293792| 2.029449| 5.422406| 1.978843|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.2764e+00| -0.052080| 2.441434| 2.177956| 5.449048| 2.676588|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.2278e+00| -0.010177| 2.533174| 2.406736| 5.485313| 4.076838|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.1956e+00| -0.052744| 2.564696| 2.541407| 5.429533| 5.993723|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.1485e+00| -0.097654| 2.574579| 2.595821| 5.377908| 7.708379|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 2.0603e+00| -0.106685| 2.574930| 2.610432| 5.380242| 8.948084|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.9810e+00| -0.109342| 2.553099| 2.619072| 5.384997| 9.841294|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.9106e+00| -0.134121| 2.493489| 2.627168| 5.354916| 10.340742|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.8648e+00| -0.176246| 2.424239| 2.620391| 5.301774| 10.424511|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.8366e+00| -0.229142| 2.367824| 2.593416| 5.240509| 10.203618|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.229142| < -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 = 0.79202 Cd = 0.077621
Cmx = 7.4e-05 Cmy = -0.202827 Cmz = 8.2e-05
Cx = 0.063787 Cy = 0.000313 Cz = 0.793254
Pressure Contribution
Cl_p = 0.79202 Cd_p = 0.077621
Cmx_p = 7.4e-05 Cmy_p = -0.202827 Cmz_p = 8.2e-05
Cx_p = 0.063787 Cy_p = 0.000313 Cz_p = 0.793254
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 0m50.280s
user 0m46.267s
sys 0m1.253s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================
delaundo: /home/jenkins/util/delaundo/delaundo/src/delaundo
=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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.
6306 grid points.
12318 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).
12318 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| 89.2595|
| CV Face Area Aspect Ratio| 1.03245| 15.7098|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6306| 1/1.00| 10|
| 1| 1816| 1/3.47| 8.04956|
| 2| 515| 1/3.53| 6.42997|
+-------------------------------------------+
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| 7.8767e-02| -1.162689| 1.074252| 1.341925| 4.312647| 0.059581|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 8.2137e-02| -1.558813| 0.823609| 0.971799| 3.926399| 0.142562|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.2595e-02| -1.590459| 0.954511| 1.033062| 3.889719| 0.379987|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 9.8957e-02| -1.655049| 0.999527| 1.039704| 3.804330| 0.969453|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 9.7306e-02| -1.667789| 0.995659| 0.974564| 3.782312| 2.384515|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 9.3619e-02| -1.633261| 0.975101| 0.867204| 3.828583| 6.281945|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 9.1210e-02| -1.618870| 0.980499| 0.834626| 3.851377| 24.415253|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 8.9100e-02| -1.640439| 1.003270| 0.896989| 3.828968| -74.351942|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.7333e-02| -1.673198| 1.016600| 0.949243| 3.790750| -27.081045|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.5976e-02| -1.692761| 1.011715| 0.949372| 3.766951| -22.709740|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.69276| < -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 = 0.81171 Cd = -0.035743
Cmz = 0.416533
Cx = -0.035743 Cy = 0.81171
Pressure Contribution
Cl_p = 0.81171 Cd_p = -0.035743
Cmz_p = 0.416533
Cx_p = -0.035743 Cy_p = 0.81171
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.327s
user 0m2.537s
sys 0m0.787s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================
pointwise: /home/jenkins/util/pointwise/PointwiseV18.5R1/pointwise
=================================================
+ echo 'su2_and_pointwise_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Traceback (most recent call last):
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_pointwise_PyTest.py", line 67, in <module>
pointwise.postAnalysis()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 6m6.389s
user 0m3.651s
sys 0m1.205s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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: 0.049587
Creating surface mesh ...
Surface mesh seconds: 0.01185
Recovering boundaries...
Boundary recovery seconds: 0.10775
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.014127
Suppressing Steiner points ...
Steiner suppression seconds: 1.2e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.021761
Refining mesh...
4188 insertions, added 2100 points, 134662 tetrahedra in queue.
1394 insertions, added 425 points, 138812 tetrahedra in queue.
1858 insertions, added 471 points, 136161 tetrahedra in queue.
2477 insertions, added 507 points, 118959 tetrahedra in queue.
3302 insertions, added 481 points, 64039 tetrahedra in queue.
4401 insertions, added 394 points, 1342 tetrahedra in queue.
Refinement seconds: 1.63582
Smoothing vertices...
Mesh smoothing seconds: 1.05639
Improving mesh...
Mesh improvement seconds: 0.066328
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006929
Total running seconds: 2.97108
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 8009
Mesh tetrahedra: 39254
Mesh faces: 81642
Mesh faces on exterior boundary: 6268
Mesh faces on input facets: 6268
Mesh edges on input segments: 9400
Steiner points on input segments: 1
Steiner points inside domain: 4869
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
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.
8009 grid points.
39254 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39254 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.09074e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 2.05157| 83.9276|
| CV Face Area Aspect Ratio| 1.31853| 36832.6|
| CV Sub-Volume Ratio| 1.0328| 1.76867e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 8009| 1/1.00| 10|
| 1| 1339| 1/5.98| 8.2634|
| 2| 221| 1/6.06| 6.79914|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.7002e-01| 0.620196| 3.052156| 2.095402| 6.111091| 1.821394|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.6251e-01| 0.861155| 3.388133| 3.046216| 6.371496| 2.187054|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.9285e-01| 0.750173| 3.392367| 3.289072| 6.260635| 3.214764|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.8165e-01| 0.570309| 3.263082| 3.330629| 6.049566| 4.586176|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.7623e-01| 0.568946| 3.182696| 3.257588| 6.036569| 5.762812|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.568946| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview |flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.75489 Cd = 0.130993
Cmx = -0.007921 Cmy = -0.211909 Cmz = 0.002289
Cx = 0.117799 Cy = 0.001444 Cz = 0.757061
real 0m8.644s
user 0m9.242s
sys 0m0.733s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_X43a_PyTest.py test;'
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 = 5653
Number of elements = 11302
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11302
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9470
Total number of elements = 18936
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 - 9470, elements - 18936
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.112308
Creating surface mesh ...
Surface mesh seconds: 0.039691
Recovering boundaries...
Warning: 4 segments are not recovered.
Boundary recovery seconds: 0.309284
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.038791
Suppressing Steiner points ...
Steiner suppression seconds: 2.4e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.044352
Refining mesh...
12627 insertions, added 5230 points, 14607 tetrahedra in queue.
Refinement seconds: 1.82745
Smoothing vertices...
Mesh smoothing seconds: 1.328
Improving mesh...
Mesh improvement seconds: 0.145123
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.021785
Total running seconds: 3.87572
Statistics:
Input points: 9470
Input facets: 18936
Input segments: 28404
Input holes: 1
Input regions: 0
Mesh points: 14908
Mesh tetrahedra: 61486
Mesh faces: 132442
Mesh faces on exterior boundary: 18940
Mesh faces on input facets: 18940
Mesh edges on input segments: 28406
Steiner points on input segments: 2
Steiner points inside domain: 5436
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.
14908 grid points.
61486 volume elements.
2 surface markers.
7638 boundary elements in index 0 (Marker = BC_1).
11302 boundary elements in index 1 (Marker = BC_2).
61486 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: 0.525713. Standard deviation K: 2.58038.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.88875| 84.097|
| CV Face Area Aspect Ratio| 1.66618| 14904.1|
| CV Sub-Volume Ratio| 1| 3.96099e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14908| 1/1.00| 10|
| 1| 2713| 1/5.5| 8.50031|
| 2| 477| 1/5.69| 7.14303|
+-------------------------------------------+
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| 5.0734e-01| 2.730418| 5.664369| 4.728196| 8.729894| -0.414116|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.9461e-01| 3.152420| 6.206734| 5.735972| 9.157575| -0.103923|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.9913e-01| 3.245709| 6.314314| 5.840624| 9.210277| -0.024348|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.9357e-01| 3.260372| 6.319757| 5.735632| 9.229075| -0.035338|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.9005e-01| 3.210996| 6.263843| 5.579934| 9.181973| -0.067136|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.211| < -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 130 non-physical points in the solution.
Warning: 48 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 = -7.183469 Cd = 106.998856
Cmx = 17.476219 Cmy = 9054.431864 Cmz = 235.6529
Cx = 107.228172 Cy = 2.07856 Cz = -1.573737
real 0m19.997s
user 0m53.183s
sys 0m1.461s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================
flowCart: /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//flowCart
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u cart3d_PyTest.py -outLevel=0
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 12:45:33 AM EST 2023
-rwx------ 1 jenkins 77175 Mar 11 00:45 ./aero.csh
CART3D env variable set to: /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28
CART3D_ARCH env variable set to: X86_64_ICC
Using codes:
-rwxrwxr-x 1 jenkins 1705984 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//cubes
-rwxrwxr-x 1 jenkins 1218584 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//mgPrep
-rwxrwxr-x 1 jenkins 4873512 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//flowCart
-rwxrwxr-x 1 jenkins 4627376 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//xsensit
-rwxrwxr-x 1 jenkins 4947568 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adjointCart
-rwxrwxr-x 1 jenkins 20755448 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adjointErrorEst_quad
-rwxrwxr-x 1 jenkins 3470040 Oct 27 2020 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adapt
md5sum checksums:
6ec5ce458d21d7844a77bdd24ec4cd67 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//cubes
eb35d7d79abba3dbf105aad946971d1e /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//mgPrep
3560020ad2308229a662deb02a126a10 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//flowCart
6c73f95283e601be7f1a6be74d0ee760 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//xsensit
adc935cc6d91afadc81adb04de12e7b0 /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adjointCart
f4550d71f2590432be4d55787b0536de /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adjointErrorEst_quad
706e383951182d9c8bc9f6393f50a31b /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//adapt
Building initial mesh
ERROR: CUBES failed in /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3dTest/Scratch/cart3dAIM0/inputs/adapt00
===> ERROR: Cannot execute cubes -- please contact Cart3D developers.
Traceback (most recent call last):
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_PyTest.py", line 61, in <module>
print ("C_A " + str(myAnalysis.output.C_A))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1950, in __getattr__
return self._capsItems[name].value
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1880, in value
return self._valObj.getValue()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================
real 0m10.567s
user 0m5.360s
sys 0m6.380s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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
(00:45:47) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
c3d_runAero.pl FAILED: aero.csh failed
Read OUT file in /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 72, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 237, in <module>
omProblem.run_driver()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/utils/hooks.py", line 131, in execute_hooks
ret = f(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/problem.py", line 686, in run_driver
return self.driver.run()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/drivers/scipy_optimizer.py", line 276, in run
model.run_solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 4678, in run_solve_nonlinear
self._solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/group.py", line 2534, in _solve_nonlinear
self._nonlinear_solver._solve_with_cache_check()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 45, in solve
self._gs_iter()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/solver.py", line 793, in _gs_iter
subsys._solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 320, in _solve_nonlinear
self._compute_wrapper()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/home/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2964, in _call_user_function
raise err_type(
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 72, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 0m18.084s
user 0m9.665s
sys 0m7.981s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
----------------------------------------
>>> 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
(00:46:02) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
c3d_runAero.pl FAILED: aero.csh failed
Read OUT file in /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 73, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 257, in <module>
omProblem.run_driver()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/utils/hooks.py", line 131, in execute_hooks
ret = f(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/problem.py", line 686, in run_driver
return self.driver.run()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/drivers/scipy_optimizer.py", line 276, in run
model.run_solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 4678, in run_solve_nonlinear
self._solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/group.py", line 2534, in _solve_nonlinear
self._nonlinear_solver._solve_with_cache_check()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/nonlinear/nonlinear_runonce.py", line 45, in solve
self._gs_iter()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/solvers/solver.py", line 793, in _gs_iter
subsys._solve_nonlinear()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 320, in _solve_nonlinear
self._compute_wrapper()
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/home/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 "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2964, in _call_user_function
raise err_type(
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/system.py", line 2958, in _call_user_function
yield
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/core/explicitcomponent.py", line 294, in _compute_wrapper
self.compute(self._inputs, self._outputs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 73, in compute
outputs['CL2'] = cart3d.dynout["CL2"].value
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1991, in value
valObj = self._analysisObj.childByName(caps.oType.VALUE, caps.sType.ANALYSISDYNO, self._name)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/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 0m11.692s
user 0m7.715s
sys 0m5.620s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/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 Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR2 : Compile Date 02/08/23 @ 12:48PM
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 Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4 : Compile Date 03/03/23 @ 11:35PM
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 = 83795
Number of elements = 489028
Number of triangles = 15694
Number of quadrilatarals = 0
Number of tetrahedrals = 473334
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 0m16.082s
user 0m15.729s
sys 0m0.690s
+ 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: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,CAPS/CFD,LINUX64,reynolds)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #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=LINUX64,buildnode=reynolds #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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