Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 49.3184| 90|
| CV Face Area Aspect Ratio| 1.00035| 33.4982|
| CV Sub-Volume Ratio| 1.00001| 7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 11153| 1/1.00| 10|
| 1| 2702| 1/4.13| 7.38309|
| 2| 549| 1/4.92| 4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 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| 7.7226e-02| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 7.5632e-02| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 7.4777e-02| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.3872e-02| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.3520e-02| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 7.3265e-02| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 7.2915e-02| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 7.2792e-02| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 7.2797e-02| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 7.2664e-02| -1.221243| 1.499646| 1.130319| 4.189559| -6.277653|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.22124| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_su2_aflr2.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file |surface_flow_pyCAPS_su2_aflr2.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary |flow_pyCAPS_su2_aflr2.szplt |
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.072253 Cd = -0.01151
Cmz = 0.070975
Cx = -0.01151 Cy = 0.072253
Pressure Contribution
Cl_p = 0.072253 Cd_p = -0.01151
Cmz_p = 0.070975
Cx_p = -0.01151 Cy_p = 0.072253
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m3.694s
user 0m3.734s
sys 0m0.998s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR4_AFLR3_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_AFLR4_AFLR3_PyTest.py test;
+ python -u su2_and_AFLR4_AFLR3_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Writing TECPLOT file: AFLR4_Mesh.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 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.5.0 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:59AM
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 11.5.8
AFLR4 : Version Date 07/24/23 @ 06:11PM
AFLR4 : Compile OS Darwin 22.5.0 x86_64
AFLR4 : Compile Date 07/25/23 @ 12:00PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.24
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.24
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 2
: MAX XYZ DEVIATION 0.0130791 TOLERANCE 0.00207194 AT NODE 14
: INPUT EDGE COORDINATE T 0.997092
: INPUT X,Y,Z COORDINATES 0, 0, 0
: EVALUATED X,Y,Z COORDINATES -0.00349719, 7.71706e-19, 0.0126029
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 4
: MAX XYZ DEVIATION 0.0105131 TOLERANCE 0.00180609 AT NODE 39
: INPUT EDGE COORDINATE T 0.995234
: INPUT X,Y,Z COORDINATES 4.56435, 7.90569, 0.137994
: EVALUATED X,Y,Z COORDINATES 4.56765, 7.90569, 0.147977
: XYZ DEVIATION > TOLERANCE AT 13 NODES ON EDGE 5
: MAX XYZ DEVIATION 0.0116919 TOLERANCE 0.00366054 AT NODE 13
: INPUT EDGE COORDINATE T 0.997249
: INPUT X,Y,Z COORDINATES 4.215, -3.14321e-19, -0.00513325
: EVALUATED X,Y,Z COORDINATES 4.2034, -2.2476e-19, -0.00367061
: XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 7
: MAX XYZ DEVIATION 0.0107541 TOLERANCE 6.07701e-05 AT NODE 39
: INPUT EDGE COORDINATE T 0.995118
: INPUT X,Y,Z COORDINATES 6.59956, 7.90569, -0.41192
: EVALUATED X,Y,Z COORDINATES 6.58881, 7.90569, -0.411568
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 12
: MAX XYZ DEVIATION 0.010541 TOLERANCE 0.00180944 AT NODE 39
: INPUT EDGE COORDINATE T 0.995222
: INPUT X,Y,Z COORDINATES 4.56435, -7.90569, 0.137994
: EVALUATED X,Y,Z COORDINATES 4.56766, -7.90569, 0.148003
: XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 14
: MAX XYZ DEVIATION 0.0107663 TOLERANCE 6.0313e-05 AT NODE 39
: INPUT EDGE COORDINATE T 0.995113
: INPUT X,Y,Z COORDINATES 6.59956, -7.90569, -0.41192
: EVALUATED X,Y,Z COORDINATES 6.5888, -7.90569, -0.411568
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 17
: MAX XYZ DEVIATION 0.0188854 TOLERANCE 0.00360043 AT NODE 5
: INPUT EDGE COORDINATE T 0.989329
: INPUT X,Y,Z COORDINATES 10, 0, 0
: EVALUATED X,Y,Z COORDINATES 9.99962, 1.15617e-18, 0.0188817
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 19
: MAX XYZ DEVIATION 0.00275272 TOLERANCE 0.000709873 AT NODE 39
: INPUT EDGE COORDINATE T 0.996882
: INPUT X,Y,Z COORDINATES 11.8257, 3.16228, 0.0551978
: EVALUATED X,Y,Z COORDINATES 11.8266, 3.16228, 0.0578281
: XYZ DEVIATION > TOLERANCE AT 5 NODES ON EDGE 20
: MAX XYZ DEVIATION 0.00942488 TOLERANCE 0.00313697 AT NODE 5
: INPUT EDGE COORDINATE T 0.994455
: INPUT X,Y,Z COORDINATES 11.686, -1.25728e-19, -0.0020533
: EVALUATED X,Y,Z COORDINATES 11.6766, -5.37476e-20, -0.000877765
: XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 22
: MAX XYZ DEVIATION 0.0026872 TOLERANCE 2.48071e-05 AT NODE 38
: INPUT EDGE COORDINATE T 0.99695
: INPUT X,Y,Z COORDINATES 12.6398, 3.16228, -0.164768
: EVALUATED X,Y,Z COORDINATES 12.6371, 3.16228, -0.164681
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 27
: MAX XYZ DEVIATION 0.00280378 TOLERANCE 0.000715677 AT NODE 39
: INPUT EDGE COORDINATE T 0.996824
: INPUT X,Y,Z COORDINATES 11.8257, -3.16228, 0.0551978
: EVALUATED X,Y,Z COORDINATES 11.8266, -3.16228, 0.0578763
: XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 29
: MAX XYZ DEVIATION 0.00266676 TOLERANCE 2.47043e-05 AT NODE 38
: INPUT EDGE COORDINATE T 0.996974
: INPUT X,Y,Z COORDINATES 12.6398, -3.16228, -0.164768
: EVALUATED X,Y,Z COORDINATES 12.6372, -3.16228, -0.164682
: XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 36
: MAX XYZ DEVIATION 0.450685 TOLERANCE 0.231543 AT NODE 11
: INPUT EDGE COORDINATE T 1.56516
: INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80
: EVALUATED X,Y,Z COORDINATES -0.450683, 5.51928e-17, 79.9987
: XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 38
: MAX XYZ DEVIATION 0.450695 TOLERANCE 0.231783 AT NODE 11
: INPUT EDGE COORDINATE T 7.84835
: INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80
: EVALUATED X,Y,Z COORDINATES 0.450694, -1.10388e-16, 79.9987
*** NON-FATAL EGADS ERROR 3299 ***
*** COORDINATES FOUND THAT DEVIATE FROM EGADS GEOMETRY ***
Volume mesh:
Number of nodes = 39312
Number of elements = 226864
Number of triangles = 12446
Number of quadrilatarals = 0
Number of tetrahedrals = 214418
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 (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.5.1 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, 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.
39312 grid points.
214418 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).
214418 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: 61.8682. 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.)| 17.1608| 84.739|
| CV Face Area Aspect Ratio| 1.11815| 37015.5|
| CV Sub-Volume Ratio| 1.04044| 455686|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 39312| 1/1.00| 10|
| 1| 6485| 1/6.06| 8.22658|
| 2| 1015| 1/6.39| 6.65012|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.038 m^2.
Area projection in the x-plane = 11.1419 m^2, y-plane = 4.96714 m^2, z-plane = 55.4182 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
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 9.4457e-01| -0.064586| 2.297676| 2.033300| 5.426310| 1.967108|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.0435e-01| -0.028142| 2.443813| 2.177084| 5.469820| 2.669025|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 8.8681e-01| 0.006388| 2.521945| 2.416533| 5.497519| 4.072698|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.8987e-01| -0.032771| 2.543134| 2.541766| 5.444377| 5.959388|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.8456e-01| -0.059484| 2.561671| 2.593774| 5.414288| 7.593451|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 8.8132e-01| -0.076814| 2.565225| 2.615896| 5.407625| 8.782803|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 8.8403e-01| -0.111978| 2.544207| 2.636258| 5.381265| 9.653546|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 8.8081e-01| -0.156369| 2.495539| 2.651467| 5.333878| 10.185394|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 8.7816e-01| -0.203072| 2.428150| 2.650114| 5.275471| 10.322264|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 8.7624e-01| -0.251896| 2.375012| 2.624886| 5.221589| 10.161308|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -0.251896| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2AFLRTest.dat |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|CSV file |surface_flow_su2AFLRTest.csv |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview |flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
|Paraview surface |surface_flow_su2AFLRTest.vtu |
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.796713 Cd = 0.078407
Cmx = 0.000211 Cmy = -0.204659 Cmz = 0.000288
Cx = 0.06449 Cy = 0.000454 Cz = 0.79796
Pressure Contribution
Cl_p = 0.796713 Cd_p = 0.078407
Cmx_p = 0.000211 Cmy_p = -0.204659 Cmz_p = 0.000288
Cx_p = 0.06449 Cy_p = 0.000454 Cz_p = 0.79796
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmx_v = 0.0 Cmy_v = 0.0 Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0 Cz_v = 0.0
real 0m34.001s
user 0m32.700s
sys 0m1.053s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================
delaundo: /Users/jenkins/util/delaundo/delaundo/src/delaundo
=================================================
+ echo 'su2_and_Delaundo_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_Delaundo_PyTest.py test;
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes be in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundoMesh.mesh
Swapping y and z coordinates!
Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file
Writing SU2 file ....
SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Warning: No boundary condition specified for capsGroup 2DSlice!
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.5.1 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_delaundoMesh.dat.
Surface file name: surface_flow_delaundoMesh.
Volume file name: flow_delaundoMesh.
Restart file name: restart_flow_delaundoMesh.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_5|
| | BC_2|
+-----------------------------------------------------------------------+
| Inlet boundary| BC_4|
+-----------------------------------------------------------------------+
| Outlet boundary| BC_3|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6320 grid points.
12346 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12346 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8142. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.3524| 89.3051|
| CV Face Area Aspect Ratio| 1.0235| 15.7138|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6320| 1/1.00| 10|
| 1| 1790| 1/3.53| 7.98287|
| 2| 504| 1/3.55| 6.35388|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104578 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 5.1957e-02| -1.163171| 1.073770| 1.341444| 4.312165| 0.062120|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 5.0896e-02| -1.561828| 0.808636| 0.967487| 3.922716| 0.139775|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 4.9823e-02| -1.601698| 0.943793| 1.009036| 3.876382| 0.373708|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 4.9565e-02| -1.659374| 1.008221| 1.015635| 3.799753| 0.952935|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.9270e-02| -1.663585| 1.011627| 0.956487| 3.788246| 2.344781|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 4.9034e-02| -1.633451| 0.991734| 0.872954| 3.829708| 6.259549|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 4.8767e-02| -1.626398| 0.990123| 0.847075| 3.843511| 26.349556|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 4.8659e-02| -1.643439| 1.009125| 0.895796| 3.825758| -56.104876|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 4.8630e-02| -1.659565| 1.020774| 0.939260| 3.804303| -24.431167|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 4.8607e-02| -1.676757| 1.012633| 0.938320| 3.783310| -21.456835|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.67676| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_delaundoMesh.dat |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|CSV file |surface_flow_delaundoMesh.csv |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary |flow_delaundoMesh.szplt |
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
|Tecplot binary surface |surface_flow_delaundoMesh.szplt |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.805231 Cd = -0.037528
Cmz = 0.414714
Cx = -0.037528 Cy = 0.805231
Pressure Contribution
Cl_p = 0.805231 Cd_p = -0.037528
Cmz_p = 0.414714
Cx_p = -0.037528 Cy_p = 0.805231
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m2.355s
user 0m2.360s
sys 0m0.909s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================
pointwise: /Applications/Pointwise/PointwiseV18.5R1/pointwise
=================================================
+ echo 'su2_and_pointwise_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Writing global Glyph inputs...
Writing egads file '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise was unable to obtain a license.
Reprise License Manager reported the following error:
pointwise: License server does not support this product (-18)
Please check your license file, network, and license server status.
Use environment variable pwid_LICENSE=port@hostname to specify a license server.
Failed to execute! (caps_system): cd '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise' && pointwise -b /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Traceback (most recent call last):
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/pyCAPS/su2_and_pointwise_PyTest.py", line 67, in <module>
pointwise.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/problem.py", line 2159, in postAnalysis
self._analysisObj.postAnalysis()
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 999, in wrapper_checkClosed
return func(*args, **kwargs)
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 2913, in postAnalysis
if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
File "/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/CAPS/pyCAPS/pyCAPS/caps.py", line 822, in _raiseStatus
raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_IOERR:
================================================================================
pointwiseAIM.c:2956 in aimPostAnalysis():
Error: Pointwise did not generate caps.GeomToMesh.ugrid or caps.GeomToMesh.lb8.ugrid!
Please make sure you are using Pointwise V18.4 or newer.
================================================================================
real 6m9.766s
user 0m6.396s
sys 0m2.337s
+ status=1
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py failed (as NOT expected)
=================================================
=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 265
Number of elements = 526
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 526
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3137
Total number of elements = 6262
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 - 3137, elements - 6262
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.049913
Creating surface mesh ...
Surface mesh seconds: 0.01198
Recovering boundaries...
Boundary recovery seconds: 0.118743
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.012734
Suppressing Steiner points ...
Steiner suppression seconds: 1.4e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.016211
Refining mesh...
4186 insertions, added 2132 points, 130189 tetrahedra in queue.
1393 insertions, added 396 points, 133609 tetrahedra in queue.
1857 insertions, added 413 points, 131356 tetrahedra in queue.
2476 insertions, added 454 points, 112928 tetrahedra in queue.
3300 insertions, added 466 points, 67068 tetrahedra in queue.
4399 insertions, added 435 points, 292 tetrahedra in queue.
5864 insertions, added 590 points, 479 tetrahedra in queue.
Refinement seconds: 1.46705
Smoothing vertices...
Mesh smoothing seconds: 0.8947
Improving mesh...
Mesh improvement seconds: 0.049439
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005133
Total running seconds: 2.62637
Statistics:
Input points: 3137
Input facets: 6262
Input segments: 9393
Input holes: 2
Input regions: 0
Mesh points: 8091
Mesh tetrahedra: 39789
Mesh faces: 82710
Mesh faces on exterior boundary: 6264
Mesh faces on input facets: 6264
Mesh edges on input segments: 9394
Steiner points on input segments: 1
Steiner points inside domain: 4953
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 (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.5.1 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, 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.
8091 grid points.
39789 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
526 boundary elements in index 2 (Marker = BC_3).
39789 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: 2.08926e+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: 30.5804. Standard deviation K: 37.5377.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.66644| 84.3027|
| CV Face Area Aspect Ratio| 1.51408| 6441.7|
| CV Sub-Volume Ratio| 1.03202| 58553.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 8091| 1/1.00| 10|
| 1| 1351| 1/5.99| 8.25992|
| 2| 223| 1/6.06| 6.79647|
+-------------------------------------------+
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
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 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| 1.6113e-01| 0.617984| 3.049944| 2.093190| 6.108879| 1.810742|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.5852e-01| 0.748911| 3.251769| 2.987153| 6.248586| 2.155825|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.5760e-01| 0.688623| 3.311837| 3.249508| 6.186781| 3.173369|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.5691e-01| 0.587426| 3.265724| 3.310895| 6.060983| 4.532123|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.5673e-01| 0.563655| 3.196458| 3.256149| 6.028232| 5.638253|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.563655| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview |flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
|Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu |
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
+-----------------------------------------------------------------------+
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.751804 Cd = 0.13334
Cmx = -0.004647 Cmy = -0.210652 Cmz = 0.001238
Cx = 0.120199 Cy = 0.000192 Cz = 0.754017
real 0m49.444s
user 0m49.600s
sys 0m0.708s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 3808
Number of elements = 7616
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7616
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 5654
Number of elements = 11304
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11304
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9462
Total number of elements = 18920
Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Number of surface: nodes - 9462, elements - 18920
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.125505
Creating surface mesh ...
Surface mesh seconds: 0.036364
Recovering boundaries...
Warning: 6 segments are not recovered.
Boundary recovery seconds: 0.300572
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.025911
Suppressing Steiner points ...
Steiner suppression seconds: 1.7e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.039785
Refining mesh...
12618 insertions, added 5287 points, 2686 tetrahedra in queue.
Refinement seconds: 1.30164
Smoothing vertices...
Mesh smoothing seconds: 1.11033
Improving mesh...
Mesh improvement seconds: 0.075372
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.011042
Total running seconds: 3.03775
Statistics:
Input points: 9462
Input facets: 18920
Input segments: 28380
Input holes: 1
Input regions: 0
Mesh points: 14838
Mesh tetrahedra: 61174
Mesh faces: 131811
Mesh faces on exterior boundary: 18926
Mesh faces on input facets: 18926
Mesh edges on input segments: 28383
Steiner points on input segments: 3
Steiner points inside domain: 5373
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 (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.5.1 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, 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.
14838 grid points.
61174 volume elements.
2 surface markers.
7622 boundary elements in index 0 (Marker = BC_1).
11304 boundary elements in index 1 (Marker = BC_2).
61174 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: 0.525156. Standard deviation K: 2.5799.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.95659| 83.8221|
| CV Face Area Aspect Ratio| 1.41663| 23894.3|
| CV Sub-Volume Ratio| 1| 751631|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14838| 1/1.00| 10|
| 1| 2667| 1/5.56| 8.46526|
| 2| 482| 1/5.53| 7.17915|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597.1 m^2.
Area projection in the x-plane = 761.677 m^2, y-plane = 2062.72 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 916077| 1| m^2/s^2| 916077|
| Velocity-X| 1189.41| 1| m/s| 1189.41|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 62.3342| 1| m/s| 62.3342|
| Velocity Magnitude| 1191.04| 1| m/s| 1191.04|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.9847e-01| 2.731555| 5.665595| 4.729268| 8.731031| -0.388627|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.8860e-01| 3.124663| 6.168534| 5.652640| 9.147040| -0.130921|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.8336e-01| 3.268952| 6.335622| 5.772165| 9.248809| -0.048395|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 2.8214e-01| 3.301113| 6.357856| 5.754955| 9.278436| -0.050401|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 2.8115e-01| 3.246860| 6.294604| 5.587733| 9.212152| -0.079853|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.24686| < -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: 84 reconstructed states for upwinding are non-physical.
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = -9.174312 Cd = 114.890297
Cmx = -22.490238 Cmy = 9469.942794 Cmz = 370.964066
Cx = 115.21299 Cy = 3.225665 Cz = -3.148845
real 0m18.328s
user 0m33.562s
sys 0m1.095s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================
./execute_PyTestRegression.sh: line 405: ulimit: stack size: cannot modify limit: Operation not permitted
flowCart: /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC//flowCart
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 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
C_A 0.050108722
C_Y -0.0015626888
C_N 0.0065057682
C_D 0.050305245
C_S -0.0015626888
C_L 0.0047530359
C_l 0.00381162
C_m -0.00346146
C_n -0.0401149
C_M_x 0.00240931
C_M_y -0.00346146
C_M_z -0.0402235
real 0m16.106s
user 0m27.446s
sys 0m0.784s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'cart3d_OpenMDAO_3_alpha_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> 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
(01:53:27) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
(01:53:29) aero.csh done
o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01631562] CL 0.12773309
----------------------------------------
----------------------------------------
>>> alpha [2.]
>>> CL2 [0.01631562] CL 0.12773309
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:53:31) Running aero.csh on 2 core(s) in M0.5901A2B0_DP1
(01:53:33) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:53:34) Linearizing cut-cells
(01:53:34) ... done
o Number of simultaneous xsensit jobs: 1
(01:53:34) Computing gradients
(01:53:38) ... done
o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01572627]]
========================================
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 1.63156D-02 |proj g|= 1.57263D-02
----------------------------------------
>>> alpha [1.98427373]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:53:39) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
(01:53:41) aero.csh done
o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.01606724] CL 0.12675617
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:53:42) Running aero.csh on 2 core(s) in M0.5901A1.98427B0_DP1
(01:53:45) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:53:45) Linearizing cut-cells
(01:53:45) ... done
o Number of simultaneous xsensit jobs: 1
(01:53:45) Computing gradients
(01:53:49) ... done
o case M0.5901A1.98427B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.01560329]]
========================================
At iterate 1 f= 1.60672D-02 |proj g|= 1.56033D-02
----------------------------------------
>>> alpha [-0.01099175]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:53:50) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
(01:53:52) aero.csh done
o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.05653687e-06] CL 0.00246101
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:53:53) Running aero.csh on 2 core(s) in M0.5901A-0.0109918B0_DP1
(01:53:56) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:53:56) Linearizing cut-cells
(01:53:56) ... done
o Number of simultaneous xsensit jobs: 1
(01:53:56) Computing gradients
(01:54:00) ... done
o case M0.5901A-0.0109918B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[0.00031042]]
========================================
At iterate 2 f= 6.05654D-06 |proj g|= 3.10424D-04
----------------------------------------
>>> alpha [-0.05149286]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:54:01) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
(01:54:04) aero.csh done
o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [2.59817201e-10] CL 1.612e-05
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:54:05) Running aero.csh on 2 core(s) in M0.5901A-0.0514929B0_DP1
(01:54:07) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:54:07) Linearizing cut-cells
(01:54:07) ... done
o Number of simultaneous xsensit jobs: 1
(01:54:07) Computing gradients
(01:54:12) ... done
o case M0.5901A-0.0514929B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[2.03612486e-06]]
========================================
At iterate 3 f= 2.59817D-10 |proj g|= 2.03612D-06
----------------------------------------
>>> alpha [-0.05176027]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:54:13) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
(01:54:15) aero.csh done
o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [9.26120217e-15] CL 1e-07
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:54:16) Running aero.csh on 2 core(s) in M0.5901A-0.0517603B0_DP1
(01:54:18) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:54:19) Linearizing cut-cells
(01:54:19) ... done
o Number of simultaneous xsensit jobs: 1
(01:54:19) Computing gradients
(01:54:23) ... done
o case M0.5901A-0.0517603B0_DP1, averaging data over 1 cycle(s)
>>> CL2_alpha [[1.21394333e-08]]
========================================
At iterate 4 f= 9.26120D-15 |proj g|= 1.21394D-08
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 4 5 4 0 0 1.214D-08 9.261D-15
F = 9.2612021713000013E-015
CONVERGENCE: NORM_OF_PROJECTED_GRADIENT_<=_PGTOL
Optimization Complete
-----------------------------------
Optimized value: [-0.05176027]
real 1m15.027s
user 0m44.953s
sys 0m9.687s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_alpha_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'cart3d_OpenMDAO_3_twist_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
----------------------------------------
>>> 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
(01:54:29) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:54:42) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00411365] CL 0.0641354
----------------------------------------
----------------------------------------
>>> twist [4.]
>>> CL2 [0.00411365] CL 0.0641354
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:54:44) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:55:02) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 37528
Estimated cutter memory: 0.003753 GB / DV
Estimated xsensit memory: 0.071303 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:55:02) Linearizing cut-cells
(01:55:04) ... done
o Number of simultaneous xsensit jobs: 1
(01:55:04) Computing gradients
(01:55:08) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00210028]]
========================================
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 1 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 4.11365D-03 |proj g|= 2.10028D-03
----------------------------------------
>>> twist [3.99789972]
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.630955
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
(01:55:13) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:55:25) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00411054] CL 0.0641174
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:55:27) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:55:47) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 37527
Estimated cutter memory: 0.003753 GB / DV
Estimated xsensit memory: 0.071301 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:55:47) Linearizing cut-cells
(01:55:49) ... done
o Number of simultaneous xsensit jobs: 1
(01:55:49) Computing gradients
(01:55:53) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[0.00209952]]
========================================
At iterate 1 f= 4.11054D-03 |proj g|= 2.09952D-03
----------------------------------------
>>> twist [-1.80638251]
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.627700
Tessellating body 1 with MaxEdge = 0.018139 Sag = 0.000907 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
(01:55:58) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:56:10) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [0.00077495] CL -0.027841
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:56:12) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:56:29) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 37739
Estimated cutter memory: 0.003774 GB / DV
Estimated xsensit memory: 0.071704 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:56:30) Linearizing cut-cells
(01:56:32) ... done
o Number of simultaneous xsensit jobs: 1
(01:56:32) Computing gradients
(01:56:36) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[-0.00093632]]
========================================
At iterate 2 f= 7.74952D-04 |proj g|= 9.36323D-04
----------------------------------------
>>> twist [-0.01621199]
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.625631
Tessellating body 1 with MaxEdge = 0.018128 Sag = 0.000906 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
(01:56:40) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:56:53) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [1.5631769e-06] CL 0.00125932
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:56:55) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:57:12) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 38636
Estimated cutter memory: 0.003864 GB / DV
Estimated xsensit memory: 0.073408 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:57:13) Linearizing cut-cells
(01:57:15) ... done
o Number of simultaneous xsensit jobs: 1
(01:57:15) Computing gradients
(01:57:19) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[4.17557661e-05]]
========================================
At iterate 3 f= 1.56318D-06 |proj g|= 4.17558D-05
----------------------------------------
>>> twist [-0.09263728]
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 3.625709
Tessellating body 1 with MaxEdge = 0.018129 Sag = 0.000906 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
(01:57:24) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:57:36) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2 [6.5457481e-07] CL 0.00081002
----------------------------------------
========================================
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:57:38) Running aero.csh on 2 core(s) in M0.5901A0B0_DP1
(01:57:56) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 37755
Estimated cutter memory: 0.003776 GB / DV
Estimated xsensit memory: 0.071735 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:57:56) Linearizing cut-cells
(01:57:58) ... done
o Number of simultaneous xsensit jobs: 1
(01:57:58) Computing gradients
(01:58:02) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
>>> CL2_twist [[2.67924265e-05]]
========================================
At iterate 4 f= 6.54575D-07 |proj g|= 2.67924D-05
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
1 4 5 4 0 0 2.679D-05 6.546D-07
F = 6.5457481049000003E-007
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized values: [-0.09263728]
real 3m39.219s
user 5m24.418s
sys 0m10.130s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'fun3d_Morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
fun3d_Morph_PyTest.py test;
+ python -u fun3d_Morph_PyTest.py -outLevel=0 -noAnalysis
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
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 9.14.7
AFLR2 : Version Date 07/16/23 @ 01:42PM
AFLR2 : Compile OS Darwin 22.5.0 x86_64
AFLR2 : Compile Date 07/25/23 @ 11:59AM
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 11.5.8
AFLR4 : Version Date 07/24/23 @ 06:11PM
AFLR4 : Compile OS Darwin 22.5.0 x86_64
AFLR4 : Compile Date 07/25/23 @ 12:00PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.24
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.24
EGADS : OpenCASCADE Version 7.6.0
EGADS : ---------------------------------------
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 2
: MAX XYZ DEVIATION 0.00694484 TOLERANCE 0.00121633 AT NODE 20
: INPUT EDGE COORDINATE T 0.998276
: INPUT X,Y,Z COORDINATES 0, 0, 0
: EVALUATED X,Y,Z COORDINATES -0.0021459, 4.04439e-19, 0.006605
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 4
: MAX XYZ DEVIATION 0.00687648 TOLERANCE 0.00131756 AT NODE 40
: INPUT EDGE COORDINATE T 0.996516
: INPUT X,Y,Z COORDINATES 4.08248, 7.07107, 0.123426
: EVALUATED X,Y,Z COORDINATES 4.08454, 7.07107, 0.129988
: XYZ DEVIATION > TOLERANCE AT 20 NODES ON EDGE 5
: MAX XYZ DEVIATION 0.00468154 TOLERANCE 0.00167181 AT NODE 20
: INPUT EDGE COORDINATE T 0.998768
: INPUT X,Y,Z COORDINATES 3.77001, -2.81137e-19, -0.00459131
: EVALUATED X,Y,Z COORDINATES 3.76537, -2.45219e-19, -0.00400473
: XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 7
: MAX XYZ DEVIATION 0.00692405 TOLERANCE 5.41787e-05 AT NODE 39
: INPUT EDGE COORDINATE T 0.996486
: INPUT X,Y,Z COORDINATES 5.90283, 7.07107, -0.368433
: EVALUATED X,Y,Z COORDINATES 5.8959, 7.07107, -0.368207
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 12
: MAX XYZ DEVIATION 0.00690409 TOLERANCE 0.00132091 AT NODE 40
: INPUT EDGE COORDINATE T 0.996502
: INPUT X,Y,Z COORDINATES 4.08248, -7.07107, 0.123426
: EVALUATED X,Y,Z COORDINATES 4.08455, -7.07107, 0.130014
: XYZ DEVIATION > TOLERANCE AT 39 NODES ON EDGE 14
: MAX XYZ DEVIATION 0.00690732 TOLERANCE 5.37685e-05 AT NODE 39
: INPUT EDGE COORDINATE T 0.996494
: INPUT X,Y,Z COORDINATES 5.90283, -7.07107, -0.368433
: EVALUATED X,Y,Z COORDINATES 5.89592, -7.07107, -0.368208
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 17
: MAX XYZ DEVIATION 0.0168917 TOLERANCE 0.00322032 AT NODE 5
: INPUT EDGE COORDINATE T 0.989329
: INPUT X,Y,Z COORDINATES 10, 0, 0
: EVALUATED X,Y,Z COORDINATES 9.99966, 1.03411e-18, 0.0168883
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 19
: MAX XYZ DEVIATION 0.0024621 TOLERANCE 0.000634929 AT NODE 39
: INPUT EDGE COORDINATE T 0.996882
: INPUT X,Y,Z COORDINATES 11.633, 2.82843, 0.0493704
: EVALUATED X,Y,Z COORDINATES 11.6337, 2.82843, 0.051723
: XYZ DEVIATION > TOLERANCE AT 5 NODES ON EDGE 20
: MAX XYZ DEVIATION 0.00842987 TOLERANCE 0.0028058 AT NODE 5
: INPUT EDGE COORDINATE T 0.994455
: INPUT X,Y,Z COORDINATES 11.508, -1.12455e-19, -0.00183653
: EVALUATED X,Y,Z COORDINATES 11.4996, -4.80733e-20, -0.000785096
: XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 22
: MAX XYZ DEVIATION 0.00240351 TOLERANCE 2.21881e-05 AT NODE 38
: INPUT EDGE COORDINATE T 0.99695
: INPUT X,Y,Z COORDINATES 12.3611, 2.82843, -0.147373
: EVALUATED X,Y,Z COORDINATES 12.3587, 2.82843, -0.147295
: XYZ DEVIATION > TOLERANCE AT 1 NODES ON EDGE 27
: MAX XYZ DEVIATION 0.00250778 TOLERANCE 0.000640121 AT NODE 39
: INPUT EDGE COORDINATE T 0.996824
: INPUT X,Y,Z COORDINATES 11.633, -2.82843, 0.0493704
: EVALUATED X,Y,Z COORDINATES 11.6337, -2.82843, 0.0517662
: XYZ DEVIATION > TOLERANCE AT 38 NODES ON EDGE 29
: MAX XYZ DEVIATION 0.00238522 TOLERANCE 2.20962e-05 AT NODE 38
: INPUT EDGE COORDINATE T 0.996974
: INPUT X,Y,Z COORDINATES 12.3611, -2.82843, -0.147373
: EVALUATED X,Y,Z COORDINATES 12.3587, -2.82843, -0.147296
: XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 32
: MAX XYZ DEVIATION 0.450685 TOLERANCE 0.231543 AT NODE 11
: INPUT EDGE COORDINATE T 1.56516
: INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80
: EVALUATED X,Y,Z COORDINATES -0.450683, 5.51928e-17, 79.9987
: XYZ DEVIATION > TOLERANCE AT 6 NODES ON EDGE 34
: MAX XYZ DEVIATION 0.450695 TOLERANCE 0.231783 AT NODE 11
: INPUT EDGE COORDINATE T 7.84835
: INPUT X,Y,Z COORDINATES 4.89859e-15, -1.19981e-30, 80
: EVALUATED X,Y,Z COORDINATES 0.450694, -1.10388e-16, 79.9987
*** NON-FATAL EGADS ERROR 3299 ***
*** COORDINATES FOUND THAT DEVIATE FROM EGADS GEOMETRY ***
Volume mesh:
Number of nodes = 79623
Number of elements = 464233
Number of triangles = 15680
Number of quadrilatarals = 0
Number of tetrahedrals = 448553
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing TECPLOT file: pyCAPS_AFLR4_AFLR3_VolMesh.dat ....
Finished writing TECPLOT file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - Alpha
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Cd2
Objective name - Const
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3dAFLRTest_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
real 0m13.034s
user 0m12.256s
sys 0m0.790s
+ 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
See pyCAPSlog.txt for more details.
=================================================
=================================================
=================================================
++ true
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.6/CAPS/CFD/DARWIN64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.6,CAPS/CFD,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #183' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.6,ESPTEST=CAPS/CFD,ESP_ARCH=DARWIN64,buildnode=macys #185'.
[Checks API] No suitable checks publisher found.
Build step 'Console output (build log) parsing' changed build result to FAILURE
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
![[Jenkins]](/csi/static/a404d988/images/svgs/logo.svg){kind=logo}
