/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl = 0.064255 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
==1681984==
==1681984== HEAP SUMMARY:
==1681984== in use at exit: 4,316,146 bytes in 24,853 blocks
==1681984== total heap usage: 707,996 allocs, 683,143 frees, 2,630,136,454 bytes allocated
==1681984==
==1681984== LEAK SUMMARY:
==1681984== definitely lost: 0 bytes in 0 blocks
==1681984== indirectly lost: 0 bytes in 0 blocks
==1681984== possibly lost: 0 bytes in 0 blocks
==1681984== still reachable: 0 bytes in 0 blocks
==1681984== suppressed: 4,316,146 bytes in 24,853 blocks
==1681984==
==1681984== For lists of detected and suppressed errors, rerun with: -s
==1681984== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4618 from 1907)
39.01user 0.94system 0:39.94elapsed 100%CPU (0avgtext+0avgdata 491484maxresident)k
784inputs+15912outputs (0major+387758minor)pagefaults 0swaps
real 0m39.944s
user 0m39.018s
sys 0m0.958s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1683858== Memcheck, a memory error detector
==1683858== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1683858== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1683858== Command: python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
==1683858==
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 11/21/22 @ 12:54PM
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 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4 : Compile Date 12/11/22 @ 11:55AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
OVERALL : CPU Time = 5.903 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
OVERALL : CPU Time = 4.832 seconds
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......
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='su2AFLRTest.cfg' mode='r' encoding='UTF-8'>
konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==1735830== Warning: invalid file descriptor 1048564 in syscall close()
==1735830== Warning: invalid file descriptor 1048565 in syscall close()
==1735830== Warning: invalid file descriptor 1048566 in syscall close()
==1735830== Warning: invalid file descriptor 1048567 in syscall close()
==1735830== Use --log-fd=<number> to select an alternative log fd.
==1735830== Warning: invalid file descriptor 1048568 in syscall close()
==1735830== Warning: invalid file descriptor 1048569 in syscall close()
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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| 1.4928e+00| -0.068489| 2.293792| 2.029449| 5.422406| 1.978843|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4891e+00| -0.052080| 2.441434| 2.177956| 5.449048| 2.676588|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.5008e+00| -0.010177| 2.533174| 2.406736| 5.485313| 4.076838|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.5039e+00| -0.052744| 2.564696| 2.541407| 5.429533| 5.993723|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.4963e+00| -0.097654| 2.574579| 2.595821| 5.377908| 7.708379|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.4920e+00| -0.106685| 2.574930| 2.610432| 5.380242| 8.948084|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.4904e+00| -0.109342| 2.553099| 2.619072| 5.384997| 9.841294|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.4816e+00| -0.134121| 2.493489| 2.627168| 5.354916| 10.340742|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.4811e+00| -0.176246| 2.424239| 2.620391| 5.301774| 10.424511|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.4801e+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) ------------------------
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl = 0.79202 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
==1683858==
==1683858== HEAP SUMMARY:
==1683858== in use at exit: 4,350,223 bytes in 24,954 blocks
==1683858== total heap usage: 1,582,064 allocs, 1,557,110 frees, 1,405,900,633 bytes allocated
==1683858==
==1683858== LEAK SUMMARY:
==1683858== definitely lost: 0 bytes in 0 blocks
==1683858== indirectly lost: 0 bytes in 0 blocks
==1683858== possibly lost: 0 bytes in 0 blocks
==1683858== still reachable: 0 bytes in 0 blocks
==1683858== suppressed: 4,350,223 bytes in 24,954 blocks
==1683858==
==1683858== For lists of detected and suppressed errors, rerun with: -s
==1683858== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1878 from 1878)
393.18user 1.46system 6:34.64elapsed 100%CPU (0avgtext+0avgdata 502812maxresident)k
0inputs+92544outputs (0major+699238minor)pagefaults 0swaps
real 6m34.649s
user 6m33.188s
sys 0m1.470s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1759685== Memcheck, a memory error detector
==1759685== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1759685== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1759685== Command: python -u su2_and_Delaundo_PyTest.py -outLevel=0
==1759685==
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......
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='delaundoMesh.cfg' mode='r' encoding='UTF-8'>
konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==1779567== Warning: invalid file descriptor 1048564 in syscall close()
==1779567== Warning: invalid file descriptor 1048565 in syscall close()
==1779567== Warning: invalid file descriptor 1048566 in syscall close()
==1779567== Warning: invalid file descriptor 1048567 in syscall close()
==1779567== Use --log-fd=<number> to select an alternative log fd.
==1779567== Warning: invalid file descriptor 1048568 in syscall close()
==1779567== Warning: invalid file descriptor 1048569 in syscall close()
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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.
6321 grid points.
12348 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).
12348 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.3524| 89.1863|
| CV Face Area Aspect Ratio| 1.01326| 15.7138|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6321| 1/1.00| 10|
| 1| 1813| 1/3.49| 8.03336|
| 2| 526| 1/3.45| 6.49056|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 7.6229e-02| -1.163205| 1.073736| 1.341410| 4.312131| 0.061871|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.5342e-02| -1.563936| 0.805914| 0.966918| 3.920134| 0.148446|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.4647e-02| -1.615354| 0.931653| 1.014748| 3.861817| 0.390941|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.4706e-02| -1.681941| 0.990139| 1.023671| 3.776977| 0.988680|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.4507e-02| -1.671275| 0.995757| 0.965712| 3.782060| 2.423105|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.4410e-02| -1.631008| 0.986777| 0.863422| 3.834311| 6.384107|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.4325e-02| -1.633603| 0.998980| 0.824803| 3.839924| 24.915712|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.4214e-02| -1.659947| 1.022883| 0.884941| 3.815491| -74.007600|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.4006e-02| -1.689092| 1.030337| 0.938389| 3.780344| -27.295508|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 7.3861e-02| -1.694679| 1.017547| 0.938628| 3.768255| -22.752401|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.69468| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_delaundoMesh.dat |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file |surface_flow_delaundoMesh.csv |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary |flow_delaundoMesh.szplt |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary surface |surface_flow_delaundoMesh.szplt |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl = 0.811253 Cd = -0.035656
Cmz = 0.414753
Cx = -0.035656 Cy = 0.811253
Pressure Contribution
Cl_p = 0.811253 Cd_p = -0.035656
Cmz_p = 0.414753
Cx_p = -0.035656 Cy_p = 0.811253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
==1759685==
==1759685== HEAP SUMMARY:
==1759685== in use at exit: 4,320,566 bytes in 24,880 blocks
==1759685== total heap usage: 648,780 allocs, 623,900 frees, 384,093,480 bytes allocated
==1759685==
==1759685== LEAK SUMMARY:
==1759685== definitely lost: 0 bytes in 0 blocks
==1759685== indirectly lost: 0 bytes in 0 blocks
==1759685== possibly lost: 0 bytes in 0 blocks
==1759685== still reachable: 0 bytes in 0 blocks
==1759685== suppressed: 4,320,566 bytes in 24,880 blocks
==1759685==
==1759685== For lists of detected and suppressed errors, rerun with: -s
==1759685== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1902 from 1902)
33.80user 0.87system 0:34.66elapsed 100%CPU (0avgtext+0avgdata 490780maxresident)k
0inputs+15080outputs (0major+308673minor)pagefaults 0swaps
real 0m34.666s
user 0m33.809s
sys 0m0.885s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1779715== Memcheck, a memory error detector
==1779715== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1779715== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1779715== Command: python -u su2_and_pointwise_PyTest.py -outLevel=0
==1779715==
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Traceback (most recent call last):
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/su2_and_pointwise_PyTest.py", line 67, in <module>
pointwise.postAnalysis()
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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.
================================================================================
==1779715==
==1779715== HEAP SUMMARY:
==1779715== in use at exit: 4,340,160 bytes in 24,908 blocks
==1779715== total heap usage: 582,380 allocs, 557,472 frees, 416,205,966 bytes allocated
==1779715==
==1779715== LEAK SUMMARY:
==1779715== definitely lost: 0 bytes in 0 blocks
==1779715== indirectly lost: 0 bytes in 0 blocks
==1779715== possibly lost: 0 bytes in 0 blocks
==1779715== still reachable: 0 bytes in 0 blocks
==1779715== suppressed: 4,340,160 bytes in 24,908 blocks
==1779715==
==1779715== For lists of detected and suppressed errors, rerun with: -s
==1779715== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1875 from 1875)
Command exited with non-zero status 1
34.63user 2.10system 6:37.57elapsed 9%CPU (0avgtext+0avgdata 305420maxresident)k
96inputs+6352outputs (0major+403585minor)pagefaults 0swaps
real 6m37.577s
user 0m34.633s
sys 0m2.115s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1797090== Memcheck, a memory error detector
==1797090== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1797090== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1797090== Command: python -u su2_and_Tetgen_PyTest.py -outLevel=0
==1797090==
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: 0.756695
Creating surface mesh ...
Surface mesh seconds: 0.129953
Recovering boundaries...
Boundary recovery seconds: 2.62632
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.138228
Suppressing Steiner points ...
Steiner suppression seconds: 0.000237
Recovering Delaunayness...
Delaunay recovery seconds: 0.305539
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: 20.0071
Smoothing vertices...
Mesh smoothing seconds: 14.2
Improving mesh...
Mesh improvement seconds: 0.292058
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.031469
Total running seconds: 38.5143
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......
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='pyCAPS_SU2_Tetgen.cfg' mode='r' encoding='UTF-8'>
konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==1809423== Warning: invalid file descriptor 1048564 in syscall close()
==1809423== Warning: invalid file descriptor 1048565 in syscall close()
==1809423== Warning: invalid file descriptor 1048566 in syscall close()
==1809423== Warning: invalid file descriptor 1048567 in syscall close()
==1809423== Use --log-fd=<number> to select an alternative log fd.
==1809423== Warning: invalid file descriptor 1048568 in syscall close()
==1809423== Warning: invalid file descriptor 1048569 in syscall close()
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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| 4.1978e-01| 0.620196| 3.052156| 2.095402| 6.111091| 1.821394|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 4.1559e-01| 0.861155| 3.388133| 3.046216| 6.371496| 2.187054|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.1394e-01| 0.750173| 3.392367| 3.289072| 6.260635| 3.214764|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.1192e-01| 0.570309| 3.263082| 3.330629| 6.049566| 4.586176|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.1091e-01| 0.568946| 3.182696| 3.257588| 6.036569| 5.762812|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.568946| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview |flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl = 0.75489 Cd = 0.130993
Cmx = -0.007921 Cmy = -0.211909 Cmz = 0.002289
Cx = 0.117799 Cy = 0.001444 Cz = 0.757061
==1797090==
==1797090== HEAP SUMMARY:
==1797090== in use at exit: 4,322,316 bytes in 24,884 blocks
==1797090== total heap usage: 942,793 allocs, 917,909 frees, 637,206,932 bytes allocated
==1797090==
==1797090== LEAK SUMMARY:
==1797090== definitely lost: 0 bytes in 0 blocks
==1797090== indirectly lost: 0 bytes in 0 blocks
==1797090== possibly lost: 0 bytes in 0 blocks
==1797090== still reachable: 0 bytes in 0 blocks
==1797090== suppressed: 4,322,316 bytes in 24,884 blocks
==1797090==
==1797090== For lists of detected and suppressed errors, rerun with: -s
==1797090== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1902 from 1902)
118.84user 1.95system 2:02.45elapsed 98%CPU (0avgtext+0avgdata 369020maxresident)k
0inputs+24048outputs (0major+577572minor)pagefaults 0swaps
real 2m2.454s
user 1m58.851s
sys 0m1.965s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1809629== Memcheck, a memory error detector
==1809629== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1809629== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1809629== Command: python -u su2_X43a_PyTest.py -outLevel=0
==1809629==
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 3808
Number of elements = 7616
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 5653
Number of elements = 11302
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11302
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9461
Total number of elements = 18918
Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Number of surface: nodes - 9461, elements - 18918
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 2.33172
Creating surface mesh ...
Surface mesh seconds: 0.569724
Recovering boundaries...
Warning: 6 segments are not recovered.
Boundary recovery seconds: 6.52718
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.258439
Suppressing Steiner points ...
Steiner suppression seconds: 0.000332
Recovering Delaunayness...
Delaunay recovery seconds: 0.760931
Refining mesh...
12616 insertions, added 5170 points, 18149 tetrahedra in queue.
Refinement seconds: 16.7672
Smoothing vertices...
Mesh smoothing seconds: 15.497
Improving mesh...
Mesh improvement seconds: 0.776992
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.100433
Total running seconds: 43.786
Statistics:
Input points: 9461
Input facets: 18918
Input segments: 28377
Input holes: 1
Input regions: 0
Mesh points: 14832
Mesh tetrahedra: 61120
Mesh faces: 131702
Mesh faces on exterior boundary: 18924
Mesh faces on input facets: 18924
Mesh edges on input segments: 28380
Steiner points on input segments: 3
Steiner points inside domain: 5368
Done meshing using TetGen!
Volume mesher did not preserve surface elements - data transfer will NOT be possible.
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......
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:142: ResourceWarning: unclosed file <_io.TextIOWrapper name='x43a_Test.cfg' mode='r' encoding='UTF-8'>
konfig = read_config(filename)
ResourceWarning: Enable tracemalloc to get the object allocation traceback
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/io/config.py:839: ResourceWarning: unclosed file <_io.TextIOWrapper name='config_CFD.cfg_tmp' mode='r' encoding='UTF-8'>
for raw_line in open(temp_filename):
ResourceWarning: Enable tracemalloc to get the object allocation traceback
==1868099== Warning: invalid file descriptor 1048564 in syscall close()
==1868099== Warning: invalid file descriptor 1048565 in syscall close()
==1868099== Warning: invalid file descriptor 1048566 in syscall close()
==1868099== Warning: invalid file descriptor 1048567 in syscall close()
==1868099== Use --log-fd=<number> to select an alternative log fd.
==1868099== Warning: invalid file descriptor 1048568 in syscall close()
==1868099== Warning: invalid file descriptor 1048569 in syscall close()
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) 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.
14832 grid points.
61120 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11302 boundary elements in index 1 (Marker = BC_2).
61120 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525189. Standard deviation K: 2.58.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.85426| 83.9017|
| CV Face Area Aspect Ratio| 1.82697| 18175.5|
| CV Sub-Volume Ratio| 1| 2.40648e+07|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14832| 1/1.00| 10|
| 1| 2681| 1/5.53| 8.48119|
| 2| 491| 1/5.46| 7.22453|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13596.7 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.48 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 916077| 1| m^2/s^2| 916077|
| Velocity-X| 1189.41| 1| m/s| 1189.41|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 62.3342| 1| m/s| 62.3342|
| Velocity Magnitude| 1191.04| 1| m/s| 1191.04|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 7.7278e-01| 2.731643| 5.665683| 4.729371| 8.731119| -0.364355|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 8.0151e-01| 3.080843| 6.131132| 5.704965| 9.099528| -0.114648|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.7875e-01| 3.239437| 6.328114| 5.859815| 9.209822| -0.043622|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.5837e-01| 3.256273| 6.326934| 5.787414| 9.235398| -0.031756|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.2366e-01| 3.158544| 6.207226| 5.618829| 9.133538| -0.051765|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.15854| < -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 127 non-physical points in the solution.
Warning: 58 reconstructed states for upwinding are non-physical.
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
/home/jenkins/util/SU2/SU2-v7.4.0/bin/SU2/run/interface.py:112: ResourceWarning: unclosed file <_io.BufferedReader name=4>
run_command( the_Command )
ResourceWarning: Enable tracemalloc to get the object allocation traceback
Total Force - Pressure + Viscous
Cl = -5.930006 Cd = 114.556586
Cmx = 39.133196 Cmy = 9163.477734 Cmz = 212.536637
Cx = 114.709943 Cy = 0.900633 Cz = 0.07355
==1809629==
==1809629== HEAP SUMMARY:
==1809629== in use at exit: 4,320,762 bytes in 24,880 blocks
==1809629== total heap usage: 5,798,900 allocs, 5,774,020 frees, 4,894,384,535 bytes allocated
==1809629==
==1809629== LEAK SUMMARY:
==1809629== definitely lost: 0 bytes in 0 blocks
==1809629== indirectly lost: 0 bytes in 0 blocks
==1809629== possibly lost: 0 bytes in 0 blocks
==1809629== still reachable: 0 bytes in 0 blocks
==1809629== suppressed: 4,320,762 bytes in 24,880 blocks
==1809629==
==1809629== For lists of detected and suppressed errors, rerun with: -s
==1809629== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1902 from 1902)
417.18user 4.30system 7:02.76elapsed 99%CPU (0avgtext+0avgdata 606556maxresident)k
0inputs+35952outputs (0major+1988988minor)pagefaults 0swaps
real 7m2.772s
user 6m57.183s
sys 0m4.317s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================
flowCart: /home/jenkins/util/cart3d/cart3d_v1.5.7_X86_64_ICC--20.10.28/bin/X86_64_ICC//flowCart
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1868412== Memcheck, a memory error detector
==1868412== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1868412== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1868412== Command: python -u cart3d_PyTest.py -outLevel=0
==1868412==
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 4 12:38:57 AM EST 2023
-rwx------ 1 jenkins 77175 Mar 4 00:38 ./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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1950, in __getattr__
return self._capsItems[name].value
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/problem.py", line 1880, in value
return self._valObj.getValue()
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1968, in getValue
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
================================================================================
==1868412==
==1868412== HEAP SUMMARY:
==1868412== in use at exit: 4,084,491 bytes in 24,439 blocks
==1868412== total heap usage: 1,180,654 allocs, 1,156,215 frees, 4,542,769,635 bytes allocated
==1868412==
==1868412== LEAK SUMMARY:
==1868412== definitely lost: 0 bytes in 0 blocks
==1868412== indirectly lost: 0 bytes in 0 blocks
==1868412== possibly lost: 0 bytes in 0 blocks
==1868412== still reachable: 0 bytes in 0 blocks
==1868412== suppressed: 4,084,491 bytes in 24,439 blocks
==1868412==
==1868412== For lists of detected and suppressed errors, rerun with: -s
==1868412== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1874 from 1874)
Command exited with non-zero status 1
78.74user 6.06system 1:24.93elapsed 99%CPU (0avgtext+0avgdata 313464maxresident)k
0inputs+11656outputs (1major+581074minor)pagefaults 0swaps
real 1m24.939s
user 1m18.749s
sys 0m6.065s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1873371== Memcheck, a memory error detector
==1873371== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1873371== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1873371== Command: python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
==1873371==
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning:
`numpy.distutils` is deprecated since NumPy 1.23.0, as a result
of the deprecation of `distutils` itself. It will be removed for
Python >= 3.12. For older Python versions it will remain present.
It is recommended to use `setuptools < 60.0` for those Python versions.
For more details, see:
https://numpy.org/devdocs/reference/distutils_status_migration.html
import numpy.distutils
----------------------------------------
>>> 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
(00:42:17) 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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py", line 237, in <module>
omProblem.run_driver()
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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/python/Python-3.9.13_valgrind/install/lib/python3.9/contextlib.py", line 137, in __exit__
self.gen.throw(typ, value, traceback)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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)
==1873371==
==1873371== HEAP SUMMARY:
==1873371== in use at exit: 6,170,969 bytes in 37,573 blocks
==1873371== total heap usage: 4,534,988 allocs, 4,497,415 frees, 5,023,243,492 bytes allocated
==1873371==
==1873371== LEAK SUMMARY:
==1873371== definitely lost: 0 bytes in 0 blocks
==1873371== indirectly lost: 0 bytes in 0 blocks
==1873371== possibly lost: 0 bytes in 0 blocks
==1873371== still reachable: 0 bytes in 0 blocks
==1873371== of which reachable via heuristic:
==1873371== stdstring : 38 bytes in 1 blocks
==1873371== suppressed: 6,170,969 bytes in 37,573 blocks
==1873371==
==1873371== For lists of detected and suppressed errors, rerun with: -s
==1873371== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4036 from 4036)
Command exited with non-zero status 1
199.46user 7.71system 3:27.39elapsed 99%CPU (0avgtext+0avgdata 524152maxresident)k
0inputs+29904outputs (0major+1076131minor)pagefaults 0swaps
real 3m27.402s
user 3m19.469s
sys 0m7.718s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1886597== Memcheck, a memory error detector
==1886597== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1886597== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1886597== Command: python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
==1886597==
/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/venv/lib/python3.9/site-packages/openmdao/components/external_code_comp.py:6: DeprecationWarning:
`numpy.distutils` is deprecated since NumPy 1.23.0, as a result
of the deprecation of `distutils` itself. It will be removed for
Python >= 3.12. For older Python versions it will remain present.
It is recommended to use `setuptools < 60.0` for those Python versions.
For more details, see:
https://numpy.org/devdocs/reference/distutils_status_migration.html
import numpy.distutils
----------------------------------------
>>> 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
(00:46:11) 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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py", line 257, in <module>
omProblem.run_driver()
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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/python/Python-3.9.13_valgrind/install/lib/python3.9/contextlib.py", line 137, in __exit__
self.gen.throw(typ, value, traceback)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/CAPS/pyCAPS/pyCAPS/caps.py", line 1331, in childByName
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/jenkins/workspace/ESP_ValgrindCaps/7.6/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)
==1886597==
==1886597== HEAP SUMMARY:
==1886597== in use at exit: 6,168,608 bytes in 37,561 blocks
==1886597== total heap usage: 4,001,212 allocs, 3,963,651 frees, 6,599,141,008 bytes allocated
==1886597==
==1886597== LEAK SUMMARY:
==1886597== definitely lost: 0 bytes in 0 blocks
==1886597== indirectly lost: 0 bytes in 0 blocks
==1886597== possibly lost: 0 bytes in 0 blocks
==1886597== still reachable: 0 bytes in 0 blocks
==1886597== of which reachable via heuristic:
==1886597== stdstring : 38 bytes in 1 blocks
==1886597== suppressed: 6,168,608 bytes in 37,561 blocks
==1886597==
==1886597== For lists of detected and suppressed errors, rerun with: -s
==1886597== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 4024 from 4024)
Command exited with non-zero status 1
225.56user 7.73system 3:53.46elapsed 99%CPU (0avgtext+0avgdata 528020maxresident)k
0inputs+32656outputs (0major+1374345minor)pagefaults 0swaps
real 3m53.468s
user 3m45.564s
sys 0m7.745s
+ 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_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ time valgrind --tool=memcheck --error-exitcode=0 --leak-check=yes --show-leak-kinds=all --keep-debuginfo=yes --gen-suppressions=all --max-stackframe=4000000 --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-AFLR.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-exodus.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-IRIT.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-MKL.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-python.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Tblade3.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-Ubuntu.supp --suppressions=/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/JenkinsESP/valgrind/valgrind-OCC7.6.supp python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
==1899513== Memcheck, a memory error detector
==1899513== Copyright (C) 2002-2017, and GNU GPL'd, by Julian Seward et al.
==1899513== Using Valgrind-3.18.1 and LibVEX; rerun with -h for copyright info
==1899513== Command: python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
==1899513==
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 11/21/22 @ 12:54PM
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 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR4 : Compile Date 12/11/22 @ 11:55AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
OVERALL : CPU Time = 6.302 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
OVERALL : CPU Time = 5.622 seconds
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
==1899513==
==1899513== HEAP SUMMARY:
==1899513== in use at exit: 4,116,907 bytes in 24,543 blocks
==1899513== total heap usage: 1,768,165 allocs, 1,743,622 frees, 1,540,763,886 bytes allocated
==1899513==
==1899513== LEAK SUMMARY:
==1899513== definitely lost: 0 bytes in 0 blocks
==1899513== indirectly lost: 0 bytes in 0 blocks
==1899513== possibly lost: 0 bytes in 0 blocks
==1899513== still reachable: 0 bytes in 0 blocks
==1899513== suppressed: 4,116,907 bytes in 24,543 blocks
==1899513==
==1899513== For lists of detected and suppressed errors, rerun with: -s
==1899513== ERROR SUMMARY: 0 errors from 0 contexts (suppressed: 1869 from 1869)
465.23user 2.11system 7:47.53elapsed 99%CPU (0avgtext+0avgdata 420924maxresident)k
0inputs+118832outputs (0major+831306minor)pagefaults 0swaps
real 7m47.540s
user 7m45.236s
sys 0m2.121s
+ 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.
=================================================
make: *** [Makefile:56: pyCAPStest] Error 1
+ exit 0
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_ValgrindCaps/7.6/CAPS/CFD/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/CFD,LINUX64,reynolds)
[Static Analysis] Using reference build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #198' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_ValgrindCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #199'.
[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] done
Finished: FAILURE
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