EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 Degen 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 Degen 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 Degen 19 19 - 18
EGADS : 36 2 Degen 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 4.21773908 0 0.00513324532
EGADS : 2 Yes 6.60185093 7.90569415 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.56435465 7.90569415 0.137994405
EGADS : 5 Yes 4.21500135 0 0
EGADS : 6 Yes 6.59955925 7.90569415 0
EGADS : 7 Yes 6.60185093 0 0
EGADS : 8 Yes 4.56435465 0 0.137994405
EGADS : 9 Yes 6.59955925 0 0
EGADS : 10 Yes 11.6870956 0 0.00205329813
EGADS : 11 Yes 12.6407404 3.16227766 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.8257419 3.16227766 0.0551977619
EGADS : 14 Yes 11.6860005 0 0
EGADS : 15 Yes 12.6398237 3.16227766 0
EGADS : 16 Yes 12.6407404 0 0
EGADS : 17 Yes 11.8257419 0 0.0551977619
EGADS : 18 Yes 12.6398237 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Writing TECPLOT file: AFLR4_Mesh_Surf_0.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: AFLR4_Mesh_Surf_1.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: AFLR4_Mesh_Surf_2.dat ....
Finished writing TECPLOT file
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
Number of surface nodes - 6280
Number of surface elements - 12548
Getting volume mesh
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.31.6
AFLR3 : Version Date 08/30/21 @ 12:37AM
AFLR3 : Compile OS Linux 3.10.0-957.27.2.el7.x86_64 x86_64
AFLR3 : Compile Date 08/30/21 @ 01:15AM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6280 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 FarField
UG3 : 2 FarField
UG3 : 3 FarField
AFLR3 : CPU Time = 0.043 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6280 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1258 7845
AFLR3 IG : Nodes, Elements = 2516 16456
AFLR3 IG : Nodes, Elements = 3774 25016
AFLR3 IG : Nodes, Elements = 5032 34242
AFLR3 IG : Nodes, Elements = 6287 43440
AFLR3 IG : Nodes, Elements = 6287 43360
AFLR3 IG : Nodes, Elements = 6280 25668
AFLR3 IG : Nodes, Elements = 6280 25683
AFLR3 IG : Nodes, Elements = 6280 20284
AFLR3 IG : Nodes, Elements = 6280 18358
AFLR3 : CPU Time = 0.354 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6280 18358
AFLR3 GG : Nodes, Elements = 9181 27275
AFLR3 GG : Nodes, Elements = 9181 39797
AFLR3 GG : Nodes, Elements = 9181 36673
AFLR3 GG : Nodes, Elements = 9181 35066
AFLR3 GG : Nodes, Elements = 11803 43267
AFLR3 GG : Nodes, Elements = 11803 54778
AFLR3 GG : Nodes, Elements = 11803 51458
AFLR3 GG : Nodes, Elements = 11803 50575
AFLR3 GG : Nodes, Elements = 14638 59334
AFLR3 GG : Nodes, Elements = 14638 71679
AFLR3 GG : Nodes, Elements = 14638 68246
AFLR3 GG : Nodes, Elements = 14638 67347
AFLR3 GG : Nodes, Elements = 17586 76354
AFLR3 GG : Nodes, Elements = 17586 89405
AFLR3 GG : Nodes, Elements = 17586 85731
AFLR3 GG : Nodes, Elements = 17586 84815
AFLR3 GG : Nodes, Elements = 20740 94422
AFLR3 GG : Nodes, Elements = 20740 108189
AFLR3 GG : Nodes, Elements = 20740 104453
AFLR3 GG : Nodes, Elements = 20740 103558
AFLR3 GG : Nodes, Elements = 24062 113621
AFLR3 GG : Nodes, Elements = 24062 127800
AFLR3 GG : Nodes, Elements = 24062 124024
AFLR3 GG : Nodes, Elements = 24062 123180
AFLR3 GG : Nodes, Elements = 27474 133516
AFLR3 GG : Nodes, Elements = 27474 148049
AFLR3 GG : Nodes, Elements = 27474 144165
AFLR3 GG : Nodes, Elements = 27474 143358
AFLR3 GG : Nodes, Elements = 30954 153880
AFLR3 GG : Nodes, Elements = 30954 168612
AFLR3 GG : Nodes, Elements = 30954 164751
AFLR3 GG : Nodes, Elements = 30954 163942
AFLR3 GG : Nodes, Elements = 34425 174420
AFLR3 GG : Nodes, Elements = 34425 189216
AFLR3 GG : Nodes, Elements = 34425 185364
AFLR3 GG : Nodes, Elements = 34425 184564
AFLR3 GG : Nodes, Elements = 37919 195091
AFLR3 GG : Nodes, Elements = 37919 209723
AFLR3 GG : Nodes, Elements = 37919 205979
AFLR3 GG : Nodes, Elements = 37919 205274
AFLR3 GG : Nodes, Elements = 41307 215488
AFLR3 GG : Nodes, Elements = 41307 229740
AFLR3 GG : Nodes, Elements = 41307 226123
AFLR3 GG : Nodes, Elements = 41307 225450
AFLR3 GG : Nodes, Elements = 44626 235439
AFLR3 GG : Nodes, Elements = 44626 249453
AFLR3 GG : Nodes, Elements = 44626 245860
AFLR3 GG : Nodes, Elements = 44626 245268
AFLR3 GG : Nodes, Elements = 47799 254806
AFLR3 GG : Nodes, Elements = 47799 268090
AFLR3 GG : Nodes, Elements = 47799 264723
AFLR3 GG : Nodes, Elements = 47799 264090
AFLR3 GG : Nodes, Elements = 50806 273120
AFLR3 GG : Nodes, Elements = 50806 285910
AFLR3 GG : Nodes, Elements = 50806 282628
AFLR3 GG : Nodes, Elements = 50806 282056
AFLR3 GG : Nodes, Elements = 53652 290607
AFLR3 GG : Nodes, Elements = 53652 302550
AFLR3 GG : Nodes, Elements = 53652 299553
AFLR3 GG : Nodes, Elements = 53652 299097
AFLR3 GG : Nodes, Elements = 56370 307256
AFLR3 GG : Nodes, Elements = 56370 318706
AFLR3 GG : Nodes, Elements = 56370 315758
AFLR3 GG : Nodes, Elements = 56370 315308
AFLR3 GG : Nodes, Elements = 58795 322585
AFLR3 GG : Nodes, Elements = 58795 332706
AFLR3 GG : Nodes, Elements = 58795 330194
AFLR3 GG : Nodes, Elements = 58795 329846
AFLR3 GG : Nodes, Elements = 60945 336298
AFLR3 GG : Nodes, Elements = 60945 345249
AFLR3 GG : Nodes, Elements = 60945 343004
AFLR3 GG : Nodes, Elements = 60945 342710
AFLR3 GG : Nodes, Elements = 62749 348126
AFLR3 GG : Nodes, Elements = 62749 355629
AFLR3 GG : Nodes, Elements = 62749 353768
AFLR3 GG : Nodes, Elements = 62749 353537
AFLR3 GG : Nodes, Elements = 64258 358065
AFLR3 GG : Nodes, Elements = 64258 364456
AFLR3 GG : Nodes, Elements = 64258 362767
AFLR3 GG : Nodes, Elements = 64258 362575
AFLR3 GG : Nodes, Elements = 65421 366069
AFLR3 GG : Nodes, Elements = 65421 371012
AFLR3 GG : Nodes, Elements = 65421 369676
AFLR3 GG : Nodes, Elements = 65421 369540
AFLR3 GG : Nodes, Elements = 66311 372210
AFLR3 GG : Nodes, Elements = 66311 375879
AFLR3 GG : Nodes, Elements = 66311 374983
AFLR3 GG : Nodes, Elements = 66311 374871
AFLR3 GG : Nodes, Elements = 66888 376602
AFLR3 GG : Nodes, Elements = 66888 379102
AFLR3 GG : Nodes, Elements = 66888 378379
AFLR3 GG : Nodes, Elements = 66888 378315
AFLR3 GG : Nodes, Elements = 67265 379448
AFLR3 GG : Nodes, Elements = 67265 381053
AFLR3 GG : Nodes, Elements = 67265 380593
AFLR3 GG : Nodes, Elements = 67265 380552
AFLR3 GG : Nodes, Elements = 67430 381047
AFLR3 GG : Nodes, Elements = 67430 381754
AFLR3 GG : Nodes, Elements = 67430 381522
AFLR3 GG : Nodes, Elements = 67430 381510
AFLR3 GG : Nodes, Elements = 67503 381729
AFLR3 GG : Nodes, Elements = 67503 382033
AFLR3 GG : Nodes, Elements = 67503 381938
AFLR3 GG : Nodes, Elements = 67503 381934
AFLR3 GG : Nodes, Elements = 67527 382006
AFLR3 GG : Nodes, Elements = 67527 382104
AFLR3 GG : Nodes, Elements = 67527 382069
AFLR3 GG : Nodes, Elements = 67527 382068
AFLR3 GG : Nodes, Elements = 67529 382074
AFLR3 GG : Nodes, Elements = 67529 382085
AFLR3 GG : Nodes, Elements = 67529 382078
AFLR3 GG : Nodes, Elements = 67531 382084
AFLR3 GG : Nodes, Elements = 67531 382090
AFLR3 GG : Nodes, Elements = 67531 382088
AFLR3 GG : Nodes, Elements = 67532 382091
AFLR3 GG : Nodes, Elements = 67532 382095
AFLR3 GG : Nodes, Elements = 67532 382093
AFLR3 GG : Nodes, Elements = 67533 382096
AFLR3 GG : Nodes, Elements = 67533 382100
AFLR3 GG : Nodes, Elements = 67533 382098
AFLR3 GG : Nodes, Elements = 67553 382158
AFLR3 GG : Nodes, Elements = 67553 382233
AFLR3 GG : Nodes, Elements = 67553 382209
AFLR3 GG : Nodes, Elements = 67553 382208
AFLR3 GG : Nodes, Elements = 67559 382226
AFLR3 GG : Nodes, Elements = 67559 382248
AFLR3 GG : Nodes, Elements = 67559 382242
AFLR3 GG : Nodes, Elements = 67560 382245
AFLR3 GG : Nodes, Elements = 67560 382250
AFLR3 GG : Nodes, Elements = 67560 382246
AFLR3 : CPU Time = 9.292 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 67560 382246
AFLR3 QI : Nodes, Elements = 66255 374854
AFLR3 QI : Nodes, Elements = 66058 373731
AFLR3 QI : Nodes, Elements = 66040 373631
AFLR3 QI : Nodes, Elements = 66038 373620
AFLR3 QI : Nodes, Elements = 66038 377219
AFLR3 QI : Nodes, Elements = 66038 373470
AFLR3 QI : Nodes, Elements = 66038 373075
AFLR3 QI : Nodes, Elements = 66038 373460
AFLR3 QI : Nodes, Elements = 66038 372866
AFLR3 QI : Nodes, Elements = 66038 372688
AFLR3 QI : Nodes, Elements = 66038 373061
AFLR3 QI : Nodes, Elements = 66038 372705
AFLR3 QI : Nodes, Elements = 66038 372678
AFLR3 QI : Nodes, Elements = 66038 372966
AFLR3 QI : Nodes, Elements = 66038 372669
AFLR3 QI : Nodes, Elements = 66038 372624
AFLR3 QI : Nodes, Elements = 66038 372890
AFLR3 QI : Nodes, Elements = 66038 372638
AFLR3 QI : Nodes, Elements = 66038 372622
AFLR3 QI : Nodes, Elements = 66047 372661
AFLR3 QI : Nodes, Elements = 66047 372939
AFLR3 QI : Nodes, Elements = 66047 372688
AFLR3 QI : Nodes, Elements = 66047 372670
AFLR3 QI : Nodes, Elements = 66047 372937
AFLR3 QI : Nodes, Elements = 66047 372690
AFLR3 QI : Nodes, Elements = 66047 372671
AFLR3 : CPU Time = 3.565 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 66047 372671
AFLR3 QRG: Nodes, Elements = 66049 372682
AFLR3 QRG: Nodes, Elements = 66050 372686
AFLR3 QRG: Nodes, Elements = 66052 372697
AFLR3 QRG: Nodes, Elements = 66060 372737
AFLR3 QRG: Nodes, Elements = 66067 372774
AFLR3 : CPU Time = 0.108 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 372774
UG3 : Min, Max Ang = 0.07909 179.4
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 45
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.08e+06
UG3 : No. Tet Elems = 372774
UG3 : Min Vol = 1.06e-09
UG3 : Average Vol = 5.59
UG3 : Total-Tet-Vol = 2.08e+06
UG3 : No. Vol<TOL = 0
UG3 : Q VOL-LENGTH-RATIO CHECK
2/3 2
UG3 : Q = c * Vol / sum( L )
UG3 : 0 <= Q <= 1
UG3 : No. Tet Elems = 372774
UG3 : Min, Max Q = 0.00948 1
UG3 : Average Q = 0.888
UG3 : No. Q< 0.1 = 23
UG3 : No. Q< 0.01 = 1
Volume mesh:
Number of nodes = 66067
Number of elements = 385322
Number of triangles = 12548
Number of quadrilatarals = 0
Number of tetrahedrals = 372774
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 - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.3.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../aflr3/aflr3_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
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_2|
+-----------------------------------------------------------------------+
| Far-field| BC_3|
+-----------------------------------------------------------------------+
| Heat flux wall| BC_1|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for 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.
66067 grid points.
372774 volume elements.
3 surface markers.
6726 boundary elements in index 0 (Marker = BC_1).
5418 boundary elements in index 1 (Marker = BC_2).
404 boundary elements in index 2 (Marker = BC_3).
372774 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.08442e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 4867.4. Mean K: 61.8716. Standard deviation K: 268.151.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 53.0047| 86.3388|
| CV Face Area Aspect Ratio| 1.05994| 89.13|
| CV Sub-Volume Ratio| 1.01898| 4648.14|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 66067| 1/1.00| 10|
| 1| 10771| 1/6.13| 8.19436|
| 2| 1635| 1/6.59| 6.55682|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 118.04 m^2.
Area projection in the x-plane = 11.1559 m^2, y-plane = 4.9782 m^2, z-plane = 55.3966 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_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.0212e+00| -0.180304| 2.586808| 2.098358| 5.310592| 4.487876|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.0022e+00| 0.096885| 2.653008| 2.278413| 5.599124| 26.324973|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 2.9652e+00| 0.130874| 2.675567| 2.397096| 5.634707| -7.079119|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.1245e+00| 0.119965| 2.658624| 2.438488| 5.621444| -3.849188|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 3.3400e+00| 0.150551| 2.629836| 2.439552| 5.645578| -3.078320|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 3.3714e+00| 0.190922| 2.627884| 2.480437| 5.682619| -3.036469|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 3.3055e+00| 0.198704| 2.624561| 2.526285| 5.682601| -3.643141|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 3.3341e+00| 0.218763| 2.627449| 2.543924| 5.700867| -4.806344|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 3.4587e+00| 0.267211| 2.647285| 2.562949| 5.740937| -4.579163|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 3.5538e+00| 0.358228| 2.719125| 2.607938| 5.823160| -8.436748|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.358228| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_su2AFLRTest.dat |
|CSV file |surface_flow_su2AFLRTest.csv |
|Paraview |flow_su2AFLRTest.vtu |
|Paraview surface |surface_flow_su2AFLRTest.vtu |
+-----------------------------------------------------------------------+
Writing the forces breakdown file (forces_breakdown_su2AFLRTest.dat).
Warning: there are 16 non-physical points in the solution.
Warning: 135 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 = 1.349161 Cd = -0.159915
Cmx = -0.024001 Cmy = -0.419415 Cmz = 0.004418
Cx = -0.183437 Cy = -0.006205 Cz = 1.346165
Pressure Contribution
Cl_p = 1.349161 Cd_p = -0.159915
Cmx_p = -0.024001 Cmy_p = -0.419415 Cmz_p = 0.004418
Cx_p = -0.183437 Cy_p = -0.006205 Cz_p = 1.346165
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 1m7.094s
user 1m1.746s
sys 0m1.644s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR4_AFLR3_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ echo 'su2_and_Delaundo_PyTest.py test;'
su2_and_Delaundo_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
+ python -u su2_and_Delaundo_PyTest.py -outLevel=0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes be in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundoMesh.mesh
Swapping y and z coordinates!
Writing TECPLOT file: delaundoMesh.dat ....
Finished writing TECPLOT file
Writing SU2 file ....
SU2 expects 2D meshes be in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Airfoil
Boundary condition name - InFlow
Boundary condition name - OutFlow
Boundary condition name - TunnelWall
Warning: No boundary condition specified for capsGroup 2DSlice!
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.3.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.
Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../delaundo/delaundoMesh.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
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 2 surfaces (outlet, inlet)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
6316 grid points.
12338 volume elements.
5 surface markers.
24 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_2).
24 boundary elements in index 3 (Marker = BC_4).
198 boundary elements in index 4 (Marker = BC_5).
12338 triangles.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
There has been a re-orientation of 294 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.917.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 1792.95. Mean K: 10.8141. Standard deviation K: 104.33.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.3524| 89.1863|
| CV Face Area Aspect Ratio| 1.01228| 15.7098|
| CV Sub-Volume Ratio| 1| 7.93643|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 6316| 1/1.00| 10|
| 1| 1836| 1/3.44| 8.08736|
| 2| 528| 1/3.48| 6.50547|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.07206 m.
Area projection in the x-plane = 0.179342 m, y-plane = 1.00053 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.138492 m.
Min. coordinate in the x-direction = -0.00104577 m, y-direction = -0.0151891 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is a single straight.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 216054| 1| m^2/s^2| 216054|
| Velocity-X| 136.119| 1| m/s| 136.119|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity Magnitude| 136.119| 1| m/s| 136.119|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.4761e-01| -1.163033| 1.073908| 1.341581| 4.312303| 0.061759|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.4542e-01| -1.559277| 0.821766| 0.974274| 3.925695| 0.143033|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.4487e-01| -1.597691| 0.952178| 1.026365| 3.881275| 0.384276|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.4454e-01| -1.665176| 1.000446| 1.033204| 3.794339| 0.985267|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.4414e-01| -1.656365| 1.003953| 0.968640| 3.797516| 2.439742|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.4388e-01| -1.625195| 0.993840| 0.865328| 3.839909| 6.566600|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.4375e-01| -1.625026| 1.001945| 0.834788| 3.848896| 28.581195|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.4372e-01| -1.650929| 1.022751| 0.893296| 3.825476| -52.880348|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.4370e-01| -1.680845| 1.030964| 0.940847| 3.791964| -24.044172|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.4370e-01| -1.693786| 1.018104| 0.935528| 3.772368| -21.085056|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| -1.69379| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_delaundoMesh.dat |
|CSV file |surface_flow_delaundoMesh.csv |
|Tecplot binary |flow_delaundoMesh.szplt |
|Tecplot binary surface |surface_flow_delaundoMesh.szplt |
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 492 more values.0: Error finishing Tecplot file output.
+-----------------------------------------------------------------------+
Writing the forces breakdown file (forces_breakdown_delaundoMesh.dat).
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.797481 Cd = -0.037822
Cmz = 0.409843
Cx = -0.037822 Cy = 0.797481
Pressure Contribution
Cl_p = 0.797481 Cd_p = -0.037822
Cmz_p = 0.409843
Cx_p = -0.037822 Cy_p = 0.797481
Viscous Contribution
Cl_v = 0.0 Cd_v = 0.0
Cmz_v = 0.0
Cx_v = 0.0 Cy_v = 0.0
real 0m4.799s
user 0m4.159s
sys 0m0.717s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_pointwise_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_pointwise_PyTest.py test;
+ python -u su2_and_pointwise_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/pyCAPS/SU2PointwiseAnalysisTest/Scratch/pointwise/caps.egads'....
Number of command line arguments = 2
Mon Jun 13 2022 1:27:08AM EDT
Pointwise V18.5
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
InitDim = 10
MaxDim = 15
MinDim = 3
TurnAngle = 0.000000
Deviation = 0.000000
SplitAngle = 0.000000
JoinCons = 0
ProxGrowthRate = 1.300000
SourceSpacing = 0
TurnAngleHard = 70.000000
EqualSpacing = 0
Domain level
Algorithm = Delaunay
FullLayers = 0
MaxLayers = 0
GrowthRate = 1.300000
IsoType = Triangle
TRexType = Triangle
TRexARLimit = 200.000000
TRexAngleBC = 0.000000
Decay = 0.500000
MinEdge = 0.000000
MaxEdge = 0.000000
Adapt = 0
WallSpacing = 0.000000
StrDomConvertARTrigger = 0.000000
Block level
Algorithm = Delaunay
VoxelLayers = 3
boundaryDecay = 0.500000
collisionBuffer = 0.500000
maxSkewAngle = 180.000000
TRexSkewDelay = 0
edgeMaxGrowthRate = 1.800000
fullLayers = 0
maxLayers = 0
growthRate = 1.300000
TRexType = TetPyramid
volInitialize = 1
General
SkipMeshing = 1
CAESolver = UGRID
outerBoxScale = 0
sourceBoxLengthScale = 0.000000
sourceBoxDirection = 1.000000 0.000000 0.000000
sourceBoxAngle = 0.000000
sourceGrowthFactor = 10.000000
sourcePCDFile =
ModelSize = 0
writeGMA = 2.0
assembleTolMult = 2.0
modelOrientIntMeshVolume = 1
Elevate On Export
degree = Q1
costThreshold = 0.8
maxIncAngle = 175.0
relax = 0.05
smoothingPasses = 1000
WCNWeight = 0.5
WCNMode = Calculate
writeVTU = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
Quilt list has 18 entries.
Quilt quilt-1: edge tolerance = 6.19984e-05
Quilt quilt-2: edge tolerance = 6.19984e-05
Quilt quilt-3: edge tolerance = 6.19984e-05
Quilt quilt-4: edge tolerance = 6.19984e-05
Quilt quilt-5: edge tolerance = 6.19984e-05
Quilt quilt-6: edge tolerance = 6.19984e-05
Quilt quilt-7: edge tolerance = 6.19984e-05
Quilt quilt-8: edge tolerance = 6.19984e-05
Quilt quilt-9: edge tolerance = 8.32902e-05
Quilt quilt-10: edge tolerance = 8.32902e-05
Quilt quilt-11: edge tolerance = 8.32902e-05
Quilt quilt-12: edge tolerance = 8.32902e-05
Quilt quilt-13: edge tolerance = 8.32902e-05
Quilt quilt-14: edge tolerance = 8.32902e-05
Quilt quilt-15: edge tolerance = 8.32902e-05
Quilt quilt-16: edge tolerance = 8.32902e-05
Quilt quilt-17: edge tolerance = 6.19601e-06
Quilt quilt-18: edge tolerance = 6.19601e-06
Maximum DB edge tolerance = 8.32902e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.665804e-04 due to model assembly tolerance
Looking for quilt names in geometry.
Quilt list has 18 entries.
Quilt list has 18 entries.
Original connector list has 32 entries.
Minimum connector length = 0.00316783
Tolerance = 8.32902e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 32 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-12
Max Edge Tol: 8.329e-05 on con-23
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/32, name = con-1
Changing dimension for connector 1/32 from 10 to 4
Checking dimension for connector 2/32, name = con-2
Checking dimension for connector 3/32, name = con-3
Changing dimension for connector 3/32 from 10 to 3
Checking dimension for connector 4/32, name = con-4
Checking dimension for connector 5/32, name = con-5
Changing dimension for connector 5/32 from 10 to 3
Checking dimension for connector 6/32, name = con-6
Changing dimension for connector 6/32 from 10 to 3
Checking dimension for connector 7/32, name = con-7
Changing dimension for connector 7/32 from 10 to 3
Checking dimension for connector 8/32, name = con-8
Checking dimension for connector 9/32, name = con-9
Changing dimension for connector 9/32 from 10 to 4
Checking dimension for connector 10/32, name = con-10
Checking dimension for connector 11/32, name = con-12
Changing dimension for connector 11/32 from 10 to 3
Checking dimension for connector 12/32, name = con-13
Checking dimension for connector 13/32, name = con-16
Changing dimension for connector 13/32 from 10 to 3
Checking dimension for connector 14/32, name = con-17
Checking dimension for connector 15/32, name = con-20
Changing dimension for connector 15/32 from 10 to 3
Checking dimension for connector 16/32, name = con-21
Changing dimension for connector 16/32 from 10 to 4
Checking dimension for connector 17/32, name = con-22
Checking dimension for connector 18/32, name = con-23
Changing dimension for connector 18/32 from 10 to 3
Checking dimension for connector 19/32, name = con-24
Checking dimension for connector 20/32, name = con-25
Changing dimension for connector 20/32 from 10 to 3
Checking dimension for connector 21/32, name = con-26
Changing dimension for connector 21/32 from 10 to 3
Checking dimension for connector 22/32, name = con-27
Changing dimension for connector 22/32 from 10 to 3
Checking dimension for connector 23/32, name = con-28
Checking dimension for connector 24/32, name = con-29
Changing dimension for connector 24/32 from 10 to 4
Checking dimension for connector 25/32, name = con-30
Checking dimension for connector 26/32, name = con-32
Changing dimension for connector 26/32 from 10 to 3
Checking dimension for connector 27/32, name = con-33
Checking dimension for connector 28/32, name = con-36
Changing dimension for connector 28/32 from 10 to 3
Checking dimension for connector 29/32, name = con-37
Checking dimension for connector 30/32, name = con-40
Changing dimension for connector 30/32 from 10 to 3
Checking dimension for connector 31/32, name = con-41
Checking dimension for connector 32/32, name = con-42
Processing spacing values for connector 1/32, name = con-1
Processing spacing values for connector 2/32, name = con-2
Processing spacing values for connector 3/32, name = con-3
Processing spacing values for connector 4/32, name = con-4
Processing spacing values for connector 5/32, name = con-5
Processing spacing values for connector 6/32, name = con-6
Processing spacing values for connector 7/32, name = con-7
Processing spacing values for connector 8/32, name = con-8
Processing spacing values for connector 9/32, name = con-9
Processing spacing values for connector 10/32, name = con-10
Processing spacing values for connector 11/32, name = con-12
Processing spacing values for connector 12/32, name = con-13
Processing spacing values for connector 13/32, name = con-16
Processing spacing values for connector 14/32, name = con-17
Processing spacing values for connector 15/32, name = con-20
Processing spacing values for connector 16/32, name = con-21
Processing spacing values for connector 17/32, name = con-22
Processing spacing values for connector 18/32, name = con-23
Processing spacing values for connector 19/32, name = con-24
Processing spacing values for connector 20/32, name = con-25
Processing spacing values for connector 21/32, name = con-26
Processing spacing values for connector 22/32, name = con-27
Processing spacing values for connector 23/32, name = con-28
Processing spacing values for connector 24/32, name = con-29
Processing spacing values for connector 25/32, name = con-30
Processing spacing values for connector 26/32, name = con-32
Processing spacing values for connector 27/32, name = con-33
Processing spacing values for connector 28/32, name = con-36
Processing spacing values for connector 29/32, name = con-37
Processing spacing values for connector 30/32, name = con-40
Processing spacing values for connector 31/32, name = con-41
Processing spacing values for connector 32/32, name = con-42
Number of unique endpoints = 20
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
Proximity test for connector 1/32, con-1.
Connector dimension changed from 4 to 15, avg. spacing changed from 1.33869 to 0.286862
Proximity test for connector 2/32, con-2.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
Proximity test for connector 3/32, con-3.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
Proximity test for connector 4/32, con-4.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
Proximity test for connector 5/32, con-5.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
Proximity test for connector 6/32, con-6.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.985232 to 0.140747
Proximity test for connector 7/32, con-7.
Proximity test for connector 8/32, con-8.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.907322 to 0.583278
Proximity test for connector 9/32, con-9.
Connector dimension changed from 4 to 15, avg. spacing changed from 1.26705 to 0.271511
Proximity test for connector 10/32, con-10.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
Proximity test for connector 11/32, con-12.
Proximity test for connector 12/32, con-13.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.821627 to 0.528189
Proximity test for connector 13/32, con-16.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.985229 to 0.140747
Proximity test for connector 14/32, con-17.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.821631 to 0.528191
Proximity test for connector 15/32, con-20.
Proximity test for connector 16/32, con-21.
Connector dimension changed from 4 to 15, avg. spacing changed from 0.535476 to 0.114745
Proximity test for connector 17/32, con-22.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
Proximity test for connector 18/32, con-23.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
Proximity test for connector 19/32, con-24.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
Proximity test for connector 20/32, con-25.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
Proximity test for connector 21/32, con-26.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.394096 to 0.0562994
Proximity test for connector 22/32, con-27.
Proximity test for connector 23/32, con-28.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.362929 to 0.233311
Proximity test for connector 24/32, con-29.
Connector dimension changed from 4 to 15, avg. spacing changed from 0.506821 to 0.108604
Proximity test for connector 25/32, con-30.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
Proximity test for connector 26/32, con-32.
Proximity test for connector 27/32, con-33.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.328651 to 0.211275
Proximity test for connector 28/32, con-36.
Connector dimension changed from 3 to 15, avg. spacing changed from 0.394092 to 0.0562988
Proximity test for connector 29/32, con-37.
Connector dimension changed from 10 to 15, avg. spacing changed from 0.328652 to 0.211277
Proximity test for connector 30/32, con-40.
Proximity test for connector 31/32, con-41.
Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
Proximity test for connector 32/32, con-42.
Connector dimension changed from 10 to 15, avg. spacing changed from 27.9253 to 17.952
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 15
Connector con-2 current dim = 15
Connector con-3 current dim = 15
Connector con-4 current dim = 15
Connector con-5 current dim = 15
Connector con-6 current dim = 15
Connector con-7 current dim = 3
Connector con-8 current dim = 15
Connector con-9 current dim = 15
Connector con-10 current dim = 15
Connector con-12 current dim = 3
Connector con-13 current dim = 15
Connector con-16 current dim = 15
Connector con-17 current dim = 15
Connector con-20 current dim = 3
Connector con-21 current dim = 15
Connector con-22 current dim = 15
Connector con-23 current dim = 15
Connector con-24 current dim = 15
Connector con-25 current dim = 15
Connector con-26 current dim = 15
Connector con-27 current dim = 3
Connector con-28 current dim = 15
Connector con-29 current dim = 15
Connector con-30 current dim = 15
Connector con-32 current dim = 3
Connector con-33 current dim = 15
Connector con-36 current dim = 15
Connector con-37 current dim = 15
Connector con-40 current dim = 3
Connector con-41 current dim = 15
Connector con-42 current dim = 15
Domain list has 18 entries.
Looking for periodic domain attributes from geometry.
Tolerance = 8.32902e-05
Number of periodic target domains = 0
Unstructured domain 1 of 18:
boundary name = Wing1.
Creating boundary name Wing1
Unstructured domain 2 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 3 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 4 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 5 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 6 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 7 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 8 of 18:
boundary name = Wing1.
Wing1 already in boundary name list.
Unstructured domain 9 of 18:
boundary name = Wing2.
Creating boundary name Wing2
Unstructured domain 10 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 11 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 12 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 13 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 14 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 15 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 16 of 18:
boundary name = Wing2.
Wing2 already in boundary name list.
Unstructured domain 17 of 18:
boundary name = Farfield.
Creating boundary name Farfield
Unstructured domain 18 of 18:
boundary name = Farfield.
Farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 18 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 18 domains.
Block = auto-blk
Setting up unstructured block.
Retrieving block attributes from geometry.
Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Mon Jun 13 2022 1:27:14AM EDT
Run Time: 00 Hours 00 Minutes 06 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Mon Jun 13 2022 1:27:14AM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 96 / 96 curves to EGADS originals
GMA contains 32 edge groups
GMA contains 18 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Mon Jun 13 2022 1:27:18AM EDT
Export Time: 00 Hours 00 Minutes 04 Seconds
Volume mesh:
Number of nodes = 16356
Number of elements = 95585
Number of triangles = 2982
Number of quadrilatarals = 0
Number of tetrahedrals = 95585
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Body = 1
Number of nodes = 547
Number of elements = 1090
Number of tris = 1090
Number of quad = 0
Body = 2
Number of nodes = 555
Number of elements = 1106
Number of tris = 1106
Number of quad = 0
Body = 3
Number of nodes = 395
Number of elements = 786
Number of tris = 786
Number of quad = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.3.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 40 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 14.1421 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_2 (0, 0, 0).
- BC_3 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_2, BC_3.
Input mesh file name: ../pointwise/caps.GeomToMesh.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_SU2_Pointwise.dat.
Surface file name: surface_flow_pyCAPS_SU2_Pointwise.
Volume file name: flow_pyCAPS_SU2_Pointwise.
Restart file name: restart_flow_pyCAPS_SU2_Pointwise.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_2|
| | BC_3|
+-----------------------------------------------------------------------+
| Far-field| BC_1|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for 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.
16356 grid points.
95585 volume elements.
3 surface markers.
786 boundary elements in index 0 (Marker = BC_1).
1090 boundary elements in index 1 (Marker = BC_2).
1106 boundary elements in index 2 (Marker = BC_3).
95585 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: 2.11289e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 6570.86. Mean K: 103.587. Standard deviation K: 505.135.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 47.0293| 82.9833|
| CV Face Area Aspect Ratio| 1.06486| 89.2124|
| CV Sub-Volume Ratio| 1.10228| 2729.83|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 16356| 1/1.00| 10|
| 1| 2589| 1/6.32| 8.11415|
| 2| 366| 1/7.07| 6.34041|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.07107 m.
Wetted area = 89.961 m^2.
Area projection in the x-plane = 8.28857 m^2, y-plane = 3.66354 m^2, z-plane = 42.3644 m^2.
Max. coordinate in the x-direction = 12.3619 m, y-direction = 7.07107 m, z-direction = 0.510646 m.
Min. coordinate in the x-direction = 0 m, y-direction = -7.07107 m, z-direction = -0.368435 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_2 is NOT a single plane.
Boundary marker BC_3 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 1.0089e+00| 0.442811| 2.860057| 2.406125| 5.933707| 2.248402|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 9.8433e-01| 0.176999| 2.668496| 2.387415| 5.662704| 2.704922|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 9.2651e-01| 0.135584| 2.666990| 2.525093| 5.611667| 3.652092|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 8.4794e-01| 0.077267| 2.655221| 2.592937| 5.549155| 4.812433|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 8.1263e-01| 0.001555| 2.649759| 2.604525| 5.479770| 5.688183|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.00155504| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Pointwise.dat|
|CSV file |surface_flow_pyCAPS_SU2_Pointwise.csv|
|Tecplot binary |flow_pyCAPS_SU2_Pointwise.szplt |
|Tecplot binary surface |surface_flow_pyCAPS_SU2_Pointwise.szplt|
+-----------------------------------------------------------------------+
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Pointwise.dat).
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.627084 Cd = 0.110243
Cmx = 0.000149 Cmy = -0.184427 Cmz = 0.000345
Cx = 0.099282 Cy = 9e-05 Cz = 0.628913
real 0m21.894s
user 0m22.652s
sys 0m2.890s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_pointwise_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_Tetgen_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_and_Tetgen_PyTest.py test;
+ python -u su2_and_Tetgen_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 2236
Number of elements = 4468
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 636
Number of elements = 1268
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 267
Number of elements = 530
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3139
Total number of elements = 6266
Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: egadsTessMesh_Surf_2.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface nodes - 3139
Number of surface elements - 6266
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds: 0.053124
Creating surface mesh ...
Surface mesh seconds: 0.012533
Recovering boundaries...
Boundary recovery seconds: 0.119163
Removing exterior tetrahedra ...
Exterior tets removal seconds: 0.009801
Suppressing Steiner points ...
Steiner suppression seconds: 1.4e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.015902
Refining mesh...
4188 insertions, added 2100 points, 134662 tetrahedra in queue.
1394 insertions, added 425 points, 138812 tetrahedra in queue.
1858 insertions, added 471 points, 136161 tetrahedra in queue.
2477 insertions, added 507 points, 118959 tetrahedra in queue.
3302 insertions, added 481 points, 64039 tetrahedra in queue.
4401 insertions, added 394 points, 1342 tetrahedra in queue.
Refinement seconds: 1.74189
Smoothing vertices...
Mesh smoothing seconds: 1.20074
Improving mesh...
Mesh improvement seconds: 0.059027
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.005513
Total running seconds: 3.2189
Statistics:
Input points: 3139
Input facets: 6266
Input segments: 9399
Input holes: 2
Input regions: 0
Mesh points: 8009
Mesh tetrahedra: 39254
Mesh faces: 81642
Mesh faces on exterior boundary: 6268
Mesh faces on input facets: 6268
Mesh edges on input segments: 9400
Steiner points on input segments: 1
Steiner points inside domain: 4869
Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.3.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5901.
Angle of attack (AoA): 1 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 50 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 15.8114 m.
Surface(s) where the force coefficients are evaluated and
their reference origin for moment computation:
- BC_1 (0, 0, 0).
- BC_2 (0, 0, 0) m.
Surface(s) plotted in the output file: BC_1, BC_2.
Input mesh file name: ../myMesh/tetgen_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
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 2 surfaces (outlet, inlet)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
8009 grid points.
39254 volume elements.
3 surface markers.
4468 boundary elements in index 0 (Marker = BC_1).
1270 boundary elements in index 1 (Marker = BC_2).
530 boundary elements in index 2 (Marker = BC_3).
39254 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.09074e+06.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 414.134. Mean K: 30.561. Standard deviation K: 37.5336.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 2.05157| 83.9276|
| CV Face Area Aspect Ratio| 1.31853| 36832.6|
| CV Sub-Volume Ratio| 1.0328| 1.76867e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 8009| 1/1.00| 10|
| 1| 1339| 1/5.98| 8.2634|
| 2| 221| 1/6.06| 6.79914|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 7.90569 m.
Wetted area = 120.046 m^2.
Area projection in the x-plane = 10.7914 m^2, y-plane = 4.58502 m^2, z-plane = 57.287 m^2.
Max. coordinate in the x-direction = 12.6407 m, y-direction = 7.90569 m, z-direction = 0.557773 m.
Min. coordinate in the x-direction = -0.00409054 m, y-direction = -7.90569 m, z-direction = -0.41192 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Boundary marker BC_2 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 226952| 1| m^2/s^2| 226952|
| Velocity-X| 200.779| 1| m/s| 200.779|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 3.50461| 1| m/s| 3.50461|
| Velocity Magnitude| 200.809| 1| m/s| 200.809|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5901|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 3.7891e-01| 0.620196| 3.052156| 2.095402| 6.111091| 1.821394|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 3.8192e-01| 0.861155| 3.388133| 3.046216| 6.371496| 2.187054|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 3.6051e-01| 0.750173| 3.392367| 3.289072| 6.260635| 3.214764|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 3.9462e-01| 0.570309| 3.263082| 3.330629| 6.049566| 4.586176|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 4.0996e-01| 0.568946| 3.182696| 3.257588| 6.036569| 5.762812|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 0.568946| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_pyCAPS_SU2_Tetgen.dat |
|CSV file |surface_flow_pyCAPS_SU2_Tetgen.csv |
|Paraview |flow_pyCAPS_SU2_Tetgen.vtu |
|Paraview surface |surface_flow_pyCAPS_SU2_Tetgen.vtu |
+-----------------------------------------------------------------------+
Writing the forces breakdown file (forces_breakdown_pyCAPS_SU2_Tetgen.dat).
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = 0.75489 Cd = 0.130993
Cmx = -0.007921 Cmy = -0.211909 Cmz = 0.002289
Cx = 0.117799 Cy = 0.001444 Cz = 0.757061
real 0m12.656s
user 0m13.155s
sys 0m0.686s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_Tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_X43a_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
su2_X43a_PyTest.py test;
+ python -u su2_X43a_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 3817
Number of elements = 7634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7634
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 5653
Number of elements = 11302
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 11302
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9470
Total number of elements = 18936
Writing TECPLOT file: egadsTessMesh_Surf_0.dat ....
Finished writing TECPLOT file
Writing TECPLOT file: egadsTessMesh_Surf_1.dat ....
Finished writing TECPLOT file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = x43A, index = 1
Name = Farfield, index = 2
Number of surface nodes - 9470
Number of surface elements - 18936
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16
Delaunizing vertices...
Delaunay seconds: 0.258427
Creating surface mesh ...
Surface mesh seconds: 0.095053
Recovering boundaries...
Warning: 4 segments are not recovered.
Boundary recovery seconds: 0.686848
Removing exterior tetrahedra ...
Exterior tets removal seconds: 0.044071
Suppressing Steiner points ...
Steiner suppression seconds: 4.1e-05
Recovering Delaunayness...
Delaunay recovery seconds: 0.094835
Refining mesh...
12627 insertions, added 5230 points, 14607 tetrahedra in queue.
Refinement seconds: 3.07331
Smoothing vertices...
Mesh smoothing seconds: 2.3804
Improving mesh...
Mesh improvement seconds: 0.211634
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.028434
Total running seconds: 6.8954
Statistics:
Input points: 9470
Input facets: 18936
Input segments: 28404
Input holes: 1
Input regions: 0
Mesh points: 14908
Mesh tetrahedra: 61486
Mesh faces: 132442
Mesh faces on exterior boundary: 18940
Mesh faces on input facets: 18940
Mesh edges on input segments: 28406
Steiner points on input segments: 2
Steiner points inside domain: 5436
Done meshing using TetGen!
Volume mesher added surface elements - data transfer will NOT be possible.
No project name ("Proj_Name") provided - A volume mesh will not be written out
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - x43A
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.3.0) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 7.3.0 "Blackbird" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2022, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 3.5.
Angle of attack (AoA): 3 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Input mesh file name: ../myMesh/tetgen_0.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
Writing solution files every 250 iterations.
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 2 surfaces (outlet, inlet)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
14908 grid points.
61486 volume elements.
2 surface markers.
7638 boundary elements in index 0 (Marker = BC_1).
11302 boundary elements in index 1 (Marker = BC_2).
61486 tetrahedra.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identifying edges and vertices.
Setting the control volume structure.
Volume of the computational grid: 2.67744e+08.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 95.6599. Mean K: 0.525713. Standard deviation K: 2.58038.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 1.88875| 84.097|
| CV Face Area Aspect Ratio| 1.66618| 14904.1|
| CV Sub-Volume Ratio| 1| 3.96099e+06|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 14908| 1/1.00| 10|
| 1| 2713| 1/5.5| 8.50031|
| 2| 477| 1/5.69| 7.14303|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 30 m.
Wetted area = 13597 m^2.
Area projection in the x-plane = 761.658 m^2, y-plane = 2062.86 m^2, z-plane = 5463.61 m^2.
Max. coordinate in the x-direction = 150 m, y-direction = 30 m, z-direction = 19 m.
Min. coordinate in the x-direction = 0 m, y-direction = -30 m, z-direction = -10.3 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_1 is NOT a single plane.
Computing wall distances.
-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.
-- Models:
+------------------------------------------------------------------------------+
| Viscosity Model| Conductivity Model| Fluid Model|
+------------------------------------------------------------------------------+
| -| -| STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Gas Constant| 287.058| 1| N.m/kg.K| 287.058|
| Spec. Heat Ratio| -| -| -| 1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
| Name| Dim. value| Ref. value| Unit|Non-dim. value|
+------------------------------------------------------------------------------+
| Static Pressure| 101325| 1| Pa| 101325|
| Density| 1.22498| 1| kg/m^3| 1.22498|
| Temperature| 288.15| 1| K| 288.15|
| Total Energy| 916077| 1| m^2/s^2| 916077|
| Velocity-X| 1189.41| 1| m/s| 1189.41|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 62.3342| 1| m/s| 62.3342|
| Velocity Magnitude| 1191.04| 1| m/s| 1191.04|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 3.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 8.5952e-01| 2.730418| 5.664369| 4.728196| 8.729894| -0.414116|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 8.7072e-01| 3.152409| 6.206724| 5.735972| 9.157568| -0.103806|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 8.4041e-01| 3.245574| 6.314099| 5.840681| 9.210175| -0.024376|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 7.5592e-01| 3.259610| 6.318662| 5.735630| 9.228374| -0.034689|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 7.5775e-01| 3.210423| 6.263802| 5.580371| 9.182001| -0.068453|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 3.21042| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_x43a_Test.dat |
|CSV file |surface_flow_x43a_Test.csv |
|Paraview |flow_x43a_Test.vtu |
|Paraview surface |surface_flow_x43a_Test.vtu |
+-----------------------------------------------------------------------+
Writing the forces breakdown file (forces_breakdown_x43a_Test.dat).
Warning: there are 128 non-physical points in the solution.
Warning: 438 reconstructed states for upwinding are non-physical.
------------------------- Solver Postprocessing -------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------
------------------------- Exit Success (SU2_CFD) ------------------------
Total Force - Pressure + Viscous
Cl = -7.325547 Cd = 107.015641
Cmx = 16.846649 Cmy = 9073.581432 Cmz = 232.830079
Cx = 107.252369 Cy = 2.055609 Cz = -1.714742
real 0m44.997s
user 1m5.890s
sys 0m1.160s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_X43a_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 7.674092
Tessellating body 1 with MaxEdge = 0.191852 Sag = 0.007674 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9 > autoInputs.out
Executing: ./aero.csh > aero.out
C_A 0.13545895
C_Y -0.0023190349
C_N 0.0017662912
C_D 0.13543807
C_S -0.0023190349
C_L -0.0029622339
C_l -0.00170699
C_m -0.00604561
C_n 0.0354751
C_M_x -0.00046789
C_M_y -0.00604561
C_M_z 0.0355131
real 0m35.130s
user 1m11.790s
sys 0m4.481s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_alpha_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_alpha_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 1
Objective name - CL2
Done getting CFD functional
Body size = 10.084180
Tessellating body 1 with MaxEdge = 0.252104 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 7 -mesh2d > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:05) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
(01:29:06) aero.csh done
o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
alpha [2.] CL2 [0.1057817] CL 0.3252412
alpha [2.] CL2 [0.1057817] CL 0.3252412
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:07) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
(01:29:10) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:29:10) Linearizing cut-cells
(01:29:10) ... done
o Number of simultaneous xsensit jobs: 1
(01:29:10) Computing gradients
(01:29:14) ... done
o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10602001]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:15) Running aero.csh on 4 core(s) in M0.5901A2B0_DP1
(01:29:19) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:29:19) Linearizing cut-cells
(01:29:19) ... done
o Number of simultaneous xsensit jobs: 1
(01:29:19) Computing gradients
(01:29:23) ... done
o case M0.5901A2B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10602001]]
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= 1.05782D-01 |proj g|= 1.06020D-01
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:24) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
(01:29:27) aero.csh done
o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
alpha [1.89397999] CL2 [0.09478706] CL 0.30787504
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:28) Running aero.csh on 4 core(s) in M0.5901A1.89398B0_DP1
(01:29:32) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:29:32) Linearizing cut-cells
(01:29:32) ... done
o Number of simultaneous xsensit jobs: 1
(01:29:32) Computing gradients
(01:29:36) ... done
o case M0.5901A1.89398B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.10074813]]
At iterate 1 f= 9.47871D-02 |proj g|= 1.00748D-01
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:37) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
(01:29:39) aero.csh done
o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
alpha [-0.13211104] CL2 [0.00047434] CL -0.02139385
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:41) Running aero.csh on 4 core(s) in M0.5901A-0.132111B0_DP1
(01:29:43) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:29:43) Linearizing cut-cells
(01:29:43) ... done
o Number of simultaneous xsensit jobs: 1
(01:29:43) Computing gradients
(01:29:47) ... done
o case M0.5901A-0.132111B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00732582]]
At iterate 2 f= 4.74339D-04 |proj g|= 7.32582D-03
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:50) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
(01:29:53) aero.csh done
o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
alpha [0.00522812] CL2 [1.32465164e-05] CL 0.00361761
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:29:56) Running aero.csh on 4 core(s) in M0.5901A0.00522812B0_DP1
(01:30:06) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:30:06) Linearizing cut-cells
(01:30:06) ... done
o Number of simultaneous xsensit jobs: 1
(01:30:06) Computing gradients
(01:30:11) ... done
o case M0.5901A0.00522812B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.001238]]
At iterate 3 f= 1.32465D-05 |proj g|= 1.23800D-03
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:13) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
(01:30:16) aero.csh done
o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01462583] CL2 [2.89471283e-05] CL -0.00546528
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:18) Running aero.csh on 4 core(s) in M0.5901A-0.0146258B0_DP1
(01:30:21) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:30:21) Linearizing cut-cells
(01:30:21) ... done
o Number of simultaneous xsensit jobs: 1
(01:30:22) Computing gradients
(01:30:26) ... done
o case M0.5901A-0.0146258B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00180066]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:27) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
(01:30:28) aero.csh done
o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
alpha [0.00067128] CL2 [8.15511616e-06] CL 0.00278569
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:29) Running aero.csh on 4 core(s) in M0.5901A0.000671285B0_DP1
(01:30:31) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:30:31) Linearizing cut-cells
(01:30:31) ... done
o Number of simultaneous xsensit jobs: 1
(01:30:31) Computing gradients
(01:30:36) ... done
o case M0.5901A0.000671285B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00097886]]
At iterate 4 f= 8.15512D-06 |proj g|= 9.78864D-04
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:37) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
(01:30:39) aero.csh done
o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01654192] CL2 [3.33627463e-05] CL -0.00584049
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:40) Running aero.csh on 4 core(s) in M0.5901A-0.0165419B0_DP1
(01:30:42) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:30:42) Linearizing cut-cells
(01:30:43) ... done
o Number of simultaneous xsensit jobs: 1
(01:30:43) Computing gradients
(01:30:47) ... done
o case M0.5901A-0.0165419B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00193604]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:49) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
(01:30:52) aero.csh done
o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00140463] CL2 [6.12816493e-06] CL 0.00237962
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:30:53) Running aero.csh on 4 core(s) in M0.5901A-0.00140463B0_DP1
(01:30:56) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:30:56) Linearizing cut-cells
(01:30:56) ... done
o Number of simultaneous xsensit jobs: 1
(01:30:56) Computing gradients
(01:31:00) ... done
o case M0.5901A-0.00140463B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00084715]]
At iterate 5 f= 6.12816D-06 |proj g|= 8.47152D-04
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:01) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
(01:31:07) aero.csh done
o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01475651] CL2 [2.9240213e-05] CL -0.00549114
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:09) Running aero.csh on 4 core(s) in M0.5901A-0.0147565B0_DP1
(01:31:13) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:31:13) Linearizing cut-cells
(01:31:13) ... done
o Number of simultaneous xsensit jobs: 1
(01:31:14) Computing gradients
(01:31:18) ... done
o case M0.5901A-0.0147565B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00181002]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:19) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
(01:31:20) aero.csh done
o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00259716] CL2 [5.08191983e-06] CL 0.002137
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:22) Running aero.csh on 4 core(s) in M0.5901A-0.00259716B0_DP1
(01:31:24) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:31:24) Linearizing cut-cells
(01:31:24) ... done
o Number of simultaneous xsensit jobs: 1
(01:31:24) Computing gradients
(01:31:28) ... done
o case M0.5901A-0.00259716B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00077084]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:30) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
(01:31:32) aero.csh done
o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00367151] CL2 [4.27119297e-06] CL 0.00192854
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:33) Running aero.csh on 4 core(s) in M0.5901A-0.00367151B0_DP1
(01:31:38) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:31:39) Linearizing cut-cells
(01:31:39) ... done
o Number of simultaneous xsensit jobs: 1
(01:31:39) Computing gradients
(01:31:43) ... done
o case M0.5901A-0.00367151B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00070603]]
At iterate 6 f= 4.27119D-06 |proj g|= 7.06030D-04
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:48) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
(01:31:56) aero.csh done
o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
alpha [-0.01501269] CL2 [2.98325477e-05] CL -0.00554238
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:31:59) Running aero.csh on 4 core(s) in M0.5901A-0.0150127B0_DP1
(01:32:06) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:32:06) Linearizing cut-cells
(01:32:06) ... done
o Number of simultaneous xsensit jobs: 1
(01:32:06) Computing gradients
(01:32:10) ... done
o case M0.5901A-0.0150127B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[-0.00182884]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:11) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
(01:32:13) aero.csh done
o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
alpha [-0.00433344] CL2 [3.77191769e-06] CL 0.00179209
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:14) Running aero.csh on 4 core(s) in M0.5901A-0.00433344B0_DP1
(01:32:16) 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: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:32:16) Linearizing cut-cells
(01:32:16) ... done
o Number of simultaneous xsensit jobs: 1
(01:32:16) Computing gradients
(01:32:20) ... done
o case M0.5901A-0.00433344B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00066572]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:21) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
(01:32:23) aero.csh done
o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
alpha [-0.004888] CL2 [3.36327638e-06] CL 0.00167372
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:24) Running aero.csh on 4 core(s) in M0.5901A-0.004888B0_DP1
(01:32:26) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 2188
Estimated cutter memory: 0.000219 GB / DV
Estimated xsensit memory: 0.004157 GB / DV
Available threads: 4
# DVs: 1
o Number of simultaneous cutter jobs: 1
(01:32:26) Linearizing cut-cells
(01:32:26) ... done
o Number of simultaneous xsensit jobs: 1
(01:32:26) Computing gradients
(01:32:30) ... done
o case M0.5901A-0.004888B0_DP1, averaging data over 1 cycle(s)
CL2_alpha [[0.00062781]]
At iterate 7 f= 3.36328D-06 |proj g|= 6.27809D-04
* * *
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 7 14 7 0 0 6.278D-04 3.363D-06
F = 3.3632763807999997E-006
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized value: [-0.004888]
real 3m31.142s
user 3m49.495s
sys 0m18.632s
+ 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 /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
cart3d_OpenMDAO_3_twist_PyTest.py test;
+ python -u cart3d_OpenMDAO_3_twist_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64/ESP/LINUX64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 1
Objective name - CL2
Done getting CFD functional
Body size = 10.084443
Tessellating body 1 with MaxEdge = 0.252111 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:34) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:32:40) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [1. 2.] CL2 [0.04745667] CL -0.217845
twist [1. 2.] CL2 [0.04745667] CL -0.217845
CAPS Info: Building sensitivity information for: twist[1,1]
CAPS Info: Building sensitivity information for: twist[2,1]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:41) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:32:49) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:32:49) Linearizing cut-cells
(01:32:51) ... done
o Number of simultaneous xsensit jobs: 2
(01:32:51) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:32:55) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02768712 0.02710382]]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:32:56) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:33:11) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:33:11) Linearizing cut-cells
(01:33:13) ... done
o Number of simultaneous xsensit jobs: 2
(01:33:13) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:33:17) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02768712 0.02710382]]
RUNNING THE L-BFGS-B CODE
* * *
Machine precision = 2.220D-16
N = 2 M = 10
At X0 0 variables are exactly at the bounds
At iterate 0 f= 4.74567D-02 |proj g|= 2.76871D-02
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 10.084443
Tessellating body 1 with MaxEdge = 0.252111 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:33:18) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:33:25) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [0.97231288 1.97289618] CL2 [0.04578804] CL -0.213981
CAPS Info: Building sensitivity information for: twist[1,1]
CAPS Info: Building sensitivity information for: twist[2,1]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:33:27) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:33:36) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:33:36) Linearizing cut-cells
(01:33:38) ... done
o Number of simultaneous xsensit jobs: 2
(01:33:38) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:33:42) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[0.02718156 0.02662519]]
At iterate 1 f= 4.57880D-02 |proj g|= 2.71816D-02
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 10.084427
Tessellating body 1 with MaxEdge = 0.252111 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:33:43) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:33:51) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.51633276 0.46520886] CL2 [2.22501294e-05] CL 0.004717
CAPS Info: Building sensitivity information for: twist[1,1]
CAPS Info: Building sensitivity information for: twist[2,1]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:33:54) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:34:01) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:34:02) Linearizing cut-cells
(01:34:04) ... done
o Number of simultaneous xsensit jobs: 2
(01:34:04) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:34:08) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[-0.00061003 -0.00059319]]
At iterate 2 f= 2.22501D-05 |proj g|= 6.10027D-04
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 10.084427
Tessellating body 1 with MaxEdge = 0.252111 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:34:12) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:34:33) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48365697 0.49806697] CL2 [5.12328397e-08] CL -0.00022635
CAPS Info: Building sensitivity information for: twist[1,1]
CAPS Info: Building sensitivity information for: twist[2,1]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:34:36) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:34:46) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:34:46) Linearizing cut-cells
(01:34:48) ... done
o Number of simultaneous xsensit jobs: 2
(01:34:49) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:34:53) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[2.92787351e-05 2.84954503e-05]]
At iterate 3 f= 5.12328D-08 |proj g|= 2.92787D-05
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing, index = 1
Body size = 10.084427
Tessellating body 1 with MaxEdge = 0.252111 Sag = 0.010084 Angle = 15.000000
Executing: autoInputs -r 30.000000 -nDiv 5 -maxR 9 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:34:54) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:35:00) aero.csh done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
twist [-0.48515345 0.49656089] CL2 [1.3228066e-09] CL -3.637e-05
CAPS Info: Building sensitivity information for: twist[1,1]
CAPS Info: Building sensitivity information for: twist[2,1]
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(01:35:02) Running aero.csh on 4 core(s) in M0.5901A0B0_DP1
(01:35:11) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 21574
Estimated cutter memory: 0.002157 GB / DV
Estimated xsensit memory: 0.040991 GB / DV
Available threads: 4
# DVs: 2
o Number of simultaneous cutter jobs: 2
(01:35:11) Linearizing cut-cells
(01:35:13) ... done
o Number of simultaneous xsensit jobs: 2
(01:35:13) Computing gradients
Adjusted OMP_NUM_THREADS to 2 for xsensit
(01:35:17) ... done
o case M0.5901A0B0_DP1, averaging data over 1 cycle(s)
CL2_twist [[4.70515011e-06 4.57923480e-06]]
At iterate 4 f= 1.32281D-09 |proj g|= 4.70515D-06
* * *
Tit = total number of iterations
Tnf = total number of function evaluations
Tnint = total number of segments explored during Cauchy searches
Skip = number of BFGS updates skipped
Nact = number of active bounds at final generalized Cauchy point
Projg = norm of the final projected gradient
F = final function value
* * *
N Tit Tnf Tnint Skip Nact Projg F
2 4 5 4 0 0 4.705D-06 1.323D-09
F = 1.3228065992000000E-009
CONVERGENCE: REL_REDUCTION_OF_F_<=_FACTR*EPSMCH
Optimization Complete
-----------------------------------
Optimized values: [-0.48515345 0.49656089]
real 2m46.865s
user 6m6.577s
sys 0m10.910s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case cart3d_OpenMDAO_3_twist_PyTest.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
Fun3D
=================================================
All tests pass!
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Sleeping for 5 seconds due to JENKINS-32191...
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/CFD/LINUX64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,CAPS/CFD,LINUX64,reynolds)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #159' 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 QualityGate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/CFD,ESP_ARCH=LINUX64,buildnode=reynolds #161'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS
![[Jenkins]](/csi/static/bc4250a1/images/svgs/logo.svg){kind=logo}
