Skipping 3,411 KB..
Full Log
AFLR3 QI : Nodes, Elements = 829589 4688438
AFLR3 QI : Nodes, Elements = 823135 4652250
AFLR3 QI : Nodes, Elements = 821238 4641520
AFLR3 QI : Nodes, Elements = 820685 4638368
AFLR3 QI : Nodes, Elements = 820541 4637549
AFLR3 QI : Nodes, Elements = 820517 4637407
AFLR3 QI : Nodes, Elements = 820510 4637366
AFLR3 QI : Nodes, Elements = 820508 4637355
AFLR3 QI : Nodes, Elements = 820508 4656485
AFLR3 QI : Nodes, Elements = 820508 4634774
AFLR3 QI : Nodes, Elements = 820508 4625695
AFLR3 QI : Nodes, Elements = 820508 4640147
AFLR3 QI : Nodes, Elements = 820508 4625558
AFLR3 QI : Nodes, Elements = 820508 4625078
AFLR3 QI : Nodes, Elements = 820508 4628468
AFLR3 QI : Nodes, Elements = 820508 4623998
AFLR3 QI : Nodes, Elements = 820508 4623361
AFLR3 QI : Nodes, Elements = 820508 4625402
AFLR3 QI : Nodes, Elements = 820508 4623121
AFLR3 QI : Nodes, Elements = 820508 4622741
AFLR3 QI : Nodes, Elements = 820508 4624403
AFLR3 QI : Nodes, Elements = 820508 4622674
AFLR3 QI : Nodes, Elements = 820508 4622390
AFLR3 QI : Nodes, Elements = 820509 4622395
AFLR3 QI : Nodes, Elements = 820509 4623873
AFLR3 QI : Nodes, Elements = 820509 4622388
AFLR3 QI : Nodes, Elements = 820509 4622360
AFLR3 QI : Nodes, Elements = 820509 4623884
AFLR3 QI : Nodes, Elements = 820509 4622359
AFLR3 QI : Nodes, Elements = 820509 4622143
AFLR3 QI : Nodes, Elements = 820509 4622395
AFLR3 : CPU Time = 25.112 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 820509 4622395
AFLR3 QRG: Nodes, Elements = 820508 4622393
AFLR3 : CPU Time = 0.820 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Ang = 6.832 164.7
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 4622393
UG3 : Min Vol = 1.8e-05
UG3 : Average Vol = 1.29e+04
UG3 : Total-Tet-Vol = 5.96e+10
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 = 4622393
UG3 : Min, Max Q = 0.0861 1
UG3 : Average Q = 0.902
UG3 : No. Q< 0.1 = 1
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 2.216 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Ang = 6.832 164.7
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 4622393
UG3 : Min Vol = 1.8e-05
UG3 : Average Vol = 1.29e+04
UG3 : Total-Tet-Vol = 5.96e+10
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 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Q = 0.252 1
UG3 : Average Q = 0.862
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
Number of nodes = 820508
Number of elements = 4774101
Number of triangles = 151708
Number of quadrilatarals = 0
Number of tetrahedrals = 4622393
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.5.
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 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 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: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-8.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| PARAVIEW| 250|
| SURFACE_PARAVIEW| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_inviscidWing.dat.
Surface file name: surface_flow_inviscidWing.
Volume file name: flow_inviscidWing.
Restart file name: restart_flow_inviscidWing.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
820508 grid points.
4622393 volume elements.
2 surface markers.
151672 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
4622393 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: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 122.726. Mean K: 4.02926. Standard deviation K: 11.9589.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.6095| 87.5269|
| CV Face Area Aspect Ratio| 1.01102| 1685.04|
| CV Sub-Volume Ratio| 1.00273| 21641.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 820508| 1/1.00| 10|
| 1| 134785| 1/6.09| 8.21506|
| 2| 20535| 1/6.56| 6.58142|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8795.17 m^2.
Area projection in the x-plane = 681.447 m^2, y-plane = 449.382 m^2, z-plane = 4224.13 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 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| 221265| 1| m^2/s^2| 221265|
| Velocity-X| 170.123| 1| m/s| 170.123|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 2.9695| 1| m/s| 2.9695|
| Velocity Magnitude| 170.149| 1| m/s| 170.149|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.5|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.1922e+01| 0.380851| 2.660758| 2.133847| 5.863696| -0.406802|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 2.0183e+01| 3.089553| 5.521554| 5.335357| 8.558356| -0.099438|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.9195e+01| 4.810028| 7.316610| 7.041831| 10.290152| 12.937512|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.8686e+01| 6.565243| 8.879480| 8.945823| 11.976242| -314.032672|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.8231e+01| 7.059342| 9.492882| 9.317846| 12.505843| 3.580064|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.8027e+01| 7.799694| 10.546869| 10.457609| 13.387376| -5.083226|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.7954e+01| 7.297248| 9.986579| 10.001935| 12.870415| 18.130588|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.7767e+01| 7.574726| 10.232539| 9.918625| 13.184939| 19.214114|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.7720e+01| 7.407586| 10.023690| 9.657584| 12.995239| 10.822917|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.7628e+01| 7.392159| 10.194699| 9.921822| 13.104957| 7.714529|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 7.39216| < -8| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_inviscidWing.dat |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|CSV file |surface_flow_inviscidWing.csv |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview |flow_inviscidWing.vtu |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
|Paraview surface |surface_flow_inviscidWing.vtu |
Writing the forces breakdown file (forces_breakdown_inviscidWing.dat).
+-----------------------------------------------------------------------+
Warning: there are 10 non-physical points in the solution.
Warning: 234 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
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 Forces and Moments
--> Cl = -36.250707 Cd = -4.699017
--> Cmx = -0.638902 Cmy = 6.00351 Cmz = -0.388151
--> Cx = -4.06564 Cy = -0.352021 Cz = -36.327195
real 7m47.730s
user 7m35.817s
sys 0m9.646s
+ status=0
+ set +x
=================================================
data/session08/2_su2_InviscidWing.py passed (as expected)
=================================================
=================================================
1_astros_ModalCantilever.py test;
+ python 1_astros_ModalCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 0.00145606
2 : 0.0014575
3 : 0.00332859
4 : 0.00333096
5 : 0.00445176
6 : 0.00445507
7 : 0.00894917
8 : 0.0089521
9 : 0.0110353
10: 0.0110413
real 1m6.534s
user 1m11.410s
sys 0m37.038s
+ status=0
+ set +x
=================================================
data/session09/1_astros_ModalCantilever.py passed (as expected)
=================================================
=================================================
2_astros_ModalSupport.py test;
+ python 2_astros_ModalSupport.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Name = ribSupport, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 831
Number of elements = 962
Number of triangle elements = 0
Number of quadrilateral elements = 962
Body 2 (of 2)
Number of nodes = 1
Number of elements = 0
Number of triangle elements = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 832
Total number of elements = 962
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = ribRootPoint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 2
Name = leftPointLoad, index = 1
Name = ritePointLoad, index = 2
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 1
Name = ribRoot, index = 1
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Name = ribSupport, index = 6
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 831
Number of elements = 962
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 962
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 832
Combined Number of elements = 963
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 962
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 6
Property name - leftWingSkin
Property name - ribSupport
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - ribRootPoint
No "constraintType" specified for Constraint tuple ribRootPoint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple ribRootPoint, going to use constraint name
Done getting FEA constraints
Getting FEA supports.......
Number of supports - 1
Support name - ribRootPoint
No "groupName" specified for Support tuple ribRootPoint, going to use support name
Done getting FEA supports
Getting FEA connections.......
Number of connection tuples - 1
Connection name - ribRoot
No "groupName" specified for Connection tuple ribRoot!
Looking for automatic connections from the use of capsConnectLink for ribRoot
9 automatic connections were made for capsConnect ribRoot (node id 832)
Done getting FEA connections
Load tuple is NULL - No loads applied
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Getting FEA analyses.......
Number of analyses - 1
Analysis name - EigenAnalysis
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing connection cards - appending mesh file
Writing Astros instruction file....
Warning: No constraints specified for case EigenAnalysis, assuming all constraints are applied!!!!
Writing analysis cards
Writing constraint cards--all constraints for each subcase
Writing support cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
==> Running mASTROS post-analysis...
Reading Astros OUT file - extracting Eigen-Values!
Number of Eigen-Values = 10
Loading Eigen-Value = 1
Loading Eigen-Value = 2
Loading Eigen-Value = 3
Loading Eigen-Value = 4
Loading Eigen-Value = 5
Loading Eigen-Value = 6
Loading Eigen-Value = 7
Loading Eigen-Value = 8
Loading Eigen-Value = 9
Loading Eigen-Value = 10
--> Eigen-frequencies:
1 : 1.93141e-08
2 : 0.0014201
3 : 0.00174471
4 : 0.00323704
5 : 0.00324327
6 : 0.00432932
7 : 0.00512433
8 : 0.00873482
9 : 0.0100619
10: 0.0107025
real 3m36.090s
user 3m27.320s
sys 1m24.241s
+ status=0
+ set +x
=================================================
data/session09/2_astros_ModalSupport.py passed (as expected)
=================================================
=================================================
3_astros_StaticCantilever.py test;
+ python 3_astros_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
==> Running mASTROS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running mASTROS post-analysis...
--> Maximum displacements:
--> Tmax 238433.3403112283
--> T1max 16861.9
--> T2max 16414.9
--> T3max 237286.0
real 0m30.122s
user 0m49.780s
sys 0m22.884s
+ status=0
+ set +x
=================================================
data/session09/3_astros_StaticCantilever.py passed (as expected)
=================================================
=================================================
4_astros_Composite.py test;
+ python 4_astros_Composite.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
==> Loading geometry from file "../ESP/transport.csm"...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
==> Running mASTROS pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Aluminum
No "materialType" specified for Material tuple Aluminum, defaulting to "Isotropic"
Material name - Graphite_epoxy
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftPointLoad
No "groupName" specified for Load tuple leftPointLoad, going to use load name
Load name - ritePointLoad
No "groupName" specified for Load tuple ritePointLoad, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Astros grid and connectivity file (in large field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS...
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running mASTROS post-analysis...
--> Maximum displacements:
--> Tmax 52594.60117638786
--> T1max 4359.68
--> T2max 3216.5
--> T3max 52322.2
real 0m29.529s
user 0m49.322s
sys 0m22.535s
+ status=0
+ set +x
=================================================
data/session09/4_astros_Composite.py passed (as expected)
=================================================
[macys.mit.edu:59822] shmem: mmap: an error occurred while determining whether or not /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T//ompi.macys.502/jf.0/2169634816/sm_segment.macys.502.81520000.0 could be created.
=================================================
6_tacs_StaticCantilever.py test;
+ python 6_tacs_StaticCantilever.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
[macys.mit.edu:59862] shmem: mmap: an error occurred while determining whether or not /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T//ompi.macys.502/jf.0/3008102400/sm_segment.macys.502.b34c0000.0 could be created.
==> Loading geometry from file "../ESP/transport.csm"...
==> Running TACS pre-analysis...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftWingSkin
No "groupName" specified for Load tuple leftWingSkin, going to use load name
Load name - riteWingSkin
No "groupName" specified for Load tuple riteWingSkin, going to use load name
Done getting FEA loads
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
[0] Creating TACSAssembler with numOwnedNodes = 425 numElements = 482
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 2.84, nnz(ILU) = 11729
==> Running TACS...
==> Running TACS post-analysis...
Tacs Analysis Outputs...
functional mass = 511406.70938906947
functional ks_vmfailure = 0.019135051727271438
real 0m31.977s
user 0m50.385s
sys 0m22.657s
+ status=0
+ set +x
=================================================
data/session09/6_tacs_StaticCantilever.py passed (as expected)
=================================================
=================================================
7_tacs_sizing.py test;
+ python 7_tacs_sizing.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
[macys.mit.edu:59888] shmem: mmap: an error occurred while determining whether or not /var/folders/xs/_fh4l1p54zqcl6mbk4zclcfr0000gp/T//ompi.macys.502/jf.0/142737408/sm_segment.macys.502.8820000.0 could be created.
==> Loading geometry from file "../ESP/transport.csm"...
==> Starting optimization...
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3852
Number of elements = 4061
Number of triangle elements = 0
Number of quadrilateral elements = 4061
----------------------------
Total number of nodes = 3852
Total number of elements = 4061
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 3852
Number of elements = 4061
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 4061
Getting FEA materials.......
Number of materials - 1
Material name - aluminum
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "groupName" specified for Constraint tuple rootConstraint, going to use constraint name
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 2
Load name - leftWingSkin
No "groupName" specified for Load tuple leftWingSkin, going to use load name
Load name - riteWingSkin
No "groupName" specified for Load tuple riteWingSkin, going to use load name
Done getting FEA loads
Getting FEA design variables.......
Number of design variables - 3
Design_Variable name - ribThk
Design_Variable name - skinThk
Design_Variable name - sparThk
Design_Variable_Relation name - relLeftSkin
Design_Variable_Relation name - relRib
Design_Variable_Relation name - relRiteSkin
Design_Variable_Relation name - relSpar
Number of design variable relations - 4
Done getting FEA design variables
Design_Constraint tuple is NULL - No design constraints applied
Design_Equation tuple is NULL - No design equations applied
Design_Table tuple is NULL - No design table constants applied
Design_Opt_Param tuple is NULL - No design optimization parameters applied
Design_Response tuple is NULL - No design responses applied
Design_Equation_Response tuple is NULL - No design equation responses applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file
Writing subElement types (if any) - appending mesh file
Writing TACS instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint ADD cards
Writing load cards
Writing constraint cards
Writing material cards
Writing property cards
Writing coordinate system cards
Writing design variable cards
Writing design variable relation cards
[0] Creating TACSAssembler with numOwnedNodes = 3852 numElements = 4061
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/data/session09/7_tacs_sizing.py:144: DeprecationWarning: Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. Ensure you extract a single element from your array before performing this operation. (Deprecated NumPy 1.25.)
xarray[ithick] = float(inputs[thick_dv])
--> ribThk [0.05]
--> skinThk [0.003]
--> sparThk [0.1]
--> mass [351348.8584378]
--> ks_vmfailure [0.18465374]
--> mass [351348.8584378]
--> ks_vmfailure [0.18465374]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00701607]]
--> ks_vmfailure skinThk [[-0.77735769]]
--> ks_vmfailure sparThk [[-0.00419852]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.00739074]
--> sparThk [0.001]
--> mass [164778.06753421]
--> ks_vmfailure [0.18458271]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.27193778]]
--> ks_vmfailure skinThk [[-0.30939956]]
--> ks_vmfailure sparThk [[-0.20978605]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.001]
--> sparThk [0.02273644]
--> mass [129232.41385728]
--> ks_vmfailure [0.20239501]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.00647627]
--> sparThk [0.00411034]
--> mass [159691.72878047]
--> ks_vmfailure [0.18468723]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.28428467]]
--> ks_vmfailure skinThk [[-0.36623707]]
--> ks_vmfailure sparThk [[-0.04561164]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.01797054]
--> skinThk [0.001]
--> sparThk [0.0012247]
--> mass [135761.31599909]
--> ks_vmfailure [0.20097431]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00336292]
--> skinThk [0.00571377]
--> sparThk [0.00370855]
--> mass [156359.73995058]
--> ks_vmfailure [0.18476613]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04724024]]
--> ks_vmfailure skinThk [[-0.42968567]]
--> ks_vmfailure sparThk [[-0.05558717]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00375419]
--> skinThk [0.0118629]
--> sparThk [0.00560564]
--> mass [221348.46889819]
--> ks_vmfailure [0.18335024]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00340205]
--> skinThk [0.00632869]
--> sparThk [0.00389826]
--> mass [162858.61284534]
--> ks_vmfailure [0.18451389]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0033671]
--> skinThk [0.00577947]
--> sparThk [0.00372882]
--> mass [157054.09556222]
--> ks_vmfailure [0.18473688]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04660765]]
--> ks_vmfailure skinThk [[-0.42085611]]
--> ks_vmfailure sparThk [[-0.05458697]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.001]
--> skinThk [0.0114244]
--> sparThk [0.01236645]
--> mass [220187.17438764]
--> ks_vmfailure [0.18349008]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.22376308]]
--> ks_vmfailure skinThk [[-0.11542908]]
--> ks_vmfailure sparThk [[-0.00924893]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00726772]
--> skinThk [0.01192034]
--> sparThk [0.01564752]
--> mass [242329.88574404]
--> ks_vmfailure [0.18318718]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00374643]
--> skinThk [0.01164171]
--> sparThk [0.01380417]
--> mass [229889.80169957]
--> ks_vmfailure [0.18327675]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0024241]
--> skinThk [0.01153708]
--> sparThk [0.01311195]
--> mass [225218.2736428]
--> ks_vmfailure [0.18333401]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04342337]]
--> ks_vmfailure skinThk [[-0.10932276]]
--> ks_vmfailure sparThk [[-0.00862543]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00273423]
--> skinThk [0.02300858]
--> sparThk [0.0208162]
--> mass [351071.64335651]
--> ks_vmfailure [0.18265072]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00246133]
--> skinThk [0.01291395]
--> sparThk [0.01403666]
--> mass [240323.86796358]
--> ks_vmfailure [0.18319035]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.04030186]]
--> ks_vmfailure skinThk [[-0.08766022]]
--> ks_vmfailure sparThk [[-0.00725048]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00615236]
--> skinThk [0.02577931]
--> sparThk [0.00214916]
--> mass [361343.31744605]
--> ks_vmfailure [0.18263733]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00640621]]
--> ks_vmfailure skinThk [[-0.02501965]]
--> ks_vmfailure sparThk [[-0.04131297]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00713229]
--> skinThk [0.02677305]
--> sparThk [0.0168223]
--> mass [392609.86291328]
--> ks_vmfailure [0.18251681]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00663017]
--> skinThk [0.02626385]
--> sparThk [0.00930372]
--> mass [376588.76116566]
--> ks_vmfailure [0.18255199]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0064128]
--> skinThk [0.02604342]
--> sparThk [0.00604892]
--> mass [369653.21087943]
--> ks_vmfailure [0.18257185]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00605012]]
--> ks_vmfailure skinThk [[-0.02434576]]
--> ks_vmfailure sparThk [[-0.00555063]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.0097372]
--> skinThk [0.04835412]
--> sparThk [0.00759194]
--> mass [602336.93932585]
--> ks_vmfailure [0.18225672]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.00752075]
--> skinThk [0.03347906]
--> sparThk [0.00656318]
--> mass [447201.32423534]
--> ks_vmfailure [0.18242234]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00423673]]
--> ks_vmfailure skinThk [[-0.01486475]]
--> ks_vmfailure sparThk [[-0.00451743]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.01240423]
--> skinThk [0.05849094]
--> sparThk [0.01317201]
--> mass [716841.47781672]
--> ks_vmfailure [0.18217976]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00154606]]
--> ks_vmfailure skinThk [[-0.00498155]]
--> ks_vmfailure sparThk [[-0.00115575]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.01929414]
--> skinThk [0.09078555]
--> sparThk [0.02029672]
--> mass [1064340.58921378]
--> ks_vmfailure [0.18206339]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00064649]]
--> ks_vmfailure skinThk [[-0.00208485]]
--> ks_vmfailure sparThk [[-0.00048511]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02545586]
--> skinThk [0.11766696]
--> sparThk [0.02722908]
--> mass [1355784.09501524]
--> ks_vmfailure [0.18201458]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0003768]]
--> ks_vmfailure skinThk [[-0.00124124]]
--> ks_vmfailure sparThk [[-0.00027327]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02816247]
--> skinThk [0.1278486]
--> sparThk [0.03061507]
--> mass [1467935.54338862]
--> ks_vmfailure [0.1820012]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00031099]]
--> ks_vmfailure skinThk [[-0.00105064]]
--> ks_vmfailure sparThk [[-0.00021913]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02874638]
--> skinThk [0.12860072]
--> sparThk [0.03166063]
--> mass [1478053.22646291]
--> ks_vmfailure [0.18200001]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00030043]]
--> ks_vmfailure skinThk [[-0.00103744]]
--> ks_vmfailure sparThk [[-0.00020726]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.02995584]
--> skinThk [0.12773274]
--> sparThk [0.03432163]
--> mass [1475323.18211848]
--> ks_vmfailure [0.18200005]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00028252]]
--> ks_vmfailure skinThk [[-0.00104812]]
--> ks_vmfailure sparThk [[-0.000184]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03300207]
--> skinThk [0.12582909]
--> sparThk [0.0407494]
--> mass [1470920.60962544]
--> ks_vmfailure [0.18200021]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00024502]]
--> ks_vmfailure skinThk [[-0.00107038]]
--> ks_vmfailure sparThk [[-0.00014848]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03417052]
--> skinThk [0.12543856]
--> sparThk [0.04303502]
--> mass [1472403.19847778]
--> ks_vmfailure [0.18200002]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00023279]]
--> ks_vmfailure skinThk [[-0.00107335]]
--> ks_vmfailure sparThk [[-0.00014019]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03466537]
--> skinThk [0.12523006]
--> sparThk [0.04393562]
--> mass [1472509.9882878]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022797]]
--> ks_vmfailure skinThk [[-0.00107536]]
--> ks_vmfailure sparThk [[-0.00013746]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03477343]
--> skinThk [0.12519386]
--> sparThk [0.04405893]
--> mass [1472530.53633059]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022693]]
--> ks_vmfailure skinThk [[-0.00107573]]
--> ks_vmfailure sparThk [[-0.00013712]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03499382]
--> skinThk [0.12513457]
--> sparThk [0.04415997]
--> mass [1472520.48038099]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022479]]
--> ks_vmfailure skinThk [[-0.00107642]]
--> ks_vmfailure sparThk [[-0.00013689]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03528602]
--> skinThk [0.12508833]
--> sparThk [0.04404571]
--> mass [1472505.62701918]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022196]]
--> ks_vmfailure skinThk [[-0.00107708]]
--> ks_vmfailure sparThk [[-0.00013735]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03554752]
--> skinThk [0.12509498]
--> sparThk [0.04357429]
--> mass [1472488.99260686]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0002194]]
--> ks_vmfailure skinThk [[-0.0010773]]
--> ks_vmfailure sparThk [[-0.00013892]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03557543]
--> skinThk [0.12515336]
--> sparThk [0.04308252]
--> mass [1472485.57497966]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00021902]]
--> ks_vmfailure skinThk [[-0.00107687]]
--> ks_vmfailure sparThk [[-0.00014054]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03549811]
--> skinThk [0.12518987]
--> sparThk [0.04292621]
--> mass [1472487.81481868]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.0002197]]
--> ks_vmfailure skinThk [[-0.00107651]]
--> ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546495]
--> skinThk [0.12519741]
--> sparThk [0.04292079]
--> mass [1472488.37514104]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022001]]
--> ks_vmfailure skinThk [[-0.00107642]]
--> ks_vmfailure sparThk [[-0.00014104]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546229]
--> skinThk [0.12519748]
--> sparThk [0.04292444]
--> mass [1472488.42506508]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022004]]
--> ks_vmfailure skinThk [[-0.00107641]]
--> ks_vmfailure sparThk [[-0.00014103]]
[0] BCSRMat: ILU(1000) Input fill ratio 20.00, actual fill ratio: 5.76, nnz(ILU) = 206656
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
--> mass [1472488.42560328]
--> ks_vmfailure [0.182]
--> mass ribThk [[2050883.76812598]]
--> mass skinThk [[10032748.6549307]]
--> mass sparThk [[1314431.32692686]]
--> ks_vmfailure ribThk [[-0.00022004]]
--> ks_vmfailure skinThk [[-0.00107641]]
--> ks_vmfailure sparThk [[-0.00014103]]
Optimization terminated successfully (Exit mode 0)
Current function value: 4.2071097874379575
Iterations: 29
Function evaluations: 39
Gradient evaluations: 29
Optimization Complete
-----------------------------------
==> Optimized value:
--> ribThk [0.03546228]
--> skinThk [0.12519745]
--> sparThk [0.0429247]
real 1m35.109s
user 1m54.815s
sys 0m24.583s
+ status=0
+ set +x
=================================================
data/session09/7_tacs_sizing.py passed (as expected)
=================================================
=================================================
2_aeroelastic_Iterative_SU2_Astros.py test;
+ python 2_aeroelastic_Iterative_SU2_Astros.py
+ tee -a /Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/CAPS/training/2023/training.log
MESSAGE:: Building wingOml
MESSAGE:: Building wingWaffle
==> Running SU2 pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Mesh sizing name - leftWing
Mesh sizing name - riteWing
Done getting mesh sizing parameters
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 21.7051
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 2651.51
AFLR4 : Abs Min Surf Spacing = 0.0542627
AFLR4 : Min Surf Spacing = 0.108525
AFLR4 : Max Surf Spacing = 2.17051
AFLR4 : Global Scale Factor = 5
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD w/BL
AFLR4 : 2 CAD geometry 0 STD w/BL
AFLR4 : 3 CAD geometry 0 STD w/BL
AFLR4 : 4 CAD geometry 0 STD w/BL
AFLR4 : 5 CAD geometry 0 STD w/BL
AFLR4 : 6 CAD geometry 0 STD w/BL
AFLR4 : 7 CAD geometry 0 STD w/BL
AFLR4 : 8 CAD geometry 0 STD w/BL
AFLR4 : 9 CAD geometry 0 STD w/BL
AFLR4 : 10 CAD geometry 0 STD w/BL
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 1107 2082 0
AFLR4 : Nodes, Trias,Quads= 685 1238 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 1473 2759 0
AFLR4 : Nodes, Trias,Quads= 721 1255 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 1116 2100 0
AFLR4 : Nodes, Trias,Quads= 671 1210 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1458 2729 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 1108 2084 0
AFLR4 : Nodes, Trias,Quads= 683 1234 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 1488 2789 0
AFLR4 : Nodes, Trias,Quads= 714 1241 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 1112 2092 0
AFLR4 : Nodes, Trias,Quads= 653 1174 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 1456 2725 0
AFLR4 : Nodes, Trias,Quads= 708 1229 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Nodes, Trias,Quads= 14 12 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 5 4 0
AFLR4 : Nodes, Trias,Quads= 4 2 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 4933 9858 1312
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 4933 9858
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 12796 24695 0
AFLR4 : Nodes, Trias,Quads= 7764 14631 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 29245 57075 0
AFLR4 : Nodes, Trias,Quads= 12448 23481 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12136 23411 0
AFLR4 : Nodes, Trias,Quads= 7447 14033 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 29424 57435 0
AFLR4 : Nodes, Trias,Quads= 12399 23385 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 12819 24741 0
AFLR4 : Nodes, Trias,Quads= 7725 14553 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 29449 57483 0
AFLR4 : Nodes, Trias,Quads= 12413 23411 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 12144 23427 0
AFLR4 : Nodes, Trias,Quads= 7471 14081 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 29445 57477 0
AFLR4 : Nodes, Trias,Quads= 12478 23543 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 196 293 0
AFLR4 : Nodes, Trias,Quads= 188 277 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 75858 151708 9398
OVERALL : CPU Time = 2.013 seconds
Body 1 (of 2)
Number of nodes = 75838
Number of elements = 151672
Number of triangle elements = 151672
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75858
Total number of elements = 151708
Total number of triangle elements = 151708
Total number of quadrilateral elements = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = leftWing, index = 1
Name = riteWing, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Wing, index = 1
Name = Farfield, index = 2
Getting volume mesh
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Darwin 23.4.0 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:29PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Darwin 23.5.0 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:21PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 2 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 10 Faces
EGADS : Body 0 has 18 Edges
EGADS : Body 0 has 10 Loops
EGADS : Body 0 has 10 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 6 Faces
EGADS : Body 1 has 12 Edges
EGADS : Body 1 has 6 Loops
EGADS : Body 1 has 8 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 6
EGADS : 2 Yes 0 0 1 1 1 1 4 5
EGADS : 3 Yes 0 0 1 1 1 1 4 8
EGADS : 4 Yes 0 0 1 1 1 2 3 5
EGADS : 5 Yes 0 0 1 1 1 2 4
EGADS : 6 Yes 0 0 1 1 1 1 7 8
EGADS : 7 Yes 0 0 1 1 1 6 9 10
EGADS : 8 Yes 0 0 1 1 1 3 6 9
EGADS : 9 Yes 0 0 1 1 1 7 8 10
EGADS : 10 Yes 0 0 1 1 1 7 9
EGADS : 11 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 12 Yes 1 0 1 NA NA 13 14 15 16
EGADS : 13 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 14 Yes 1 0 1 NA NA 11 12 15 16
EGADS : 15 Yes 1 0 1 NA NA 11 12 13 14
EGADS : 16 Yes 1 0 1 NA NA 11 12 13 14
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 -1 2 3 -4
EGADS : 2 -5 4 6 -7
EGADS : 3 -3 8 1 -9
EGADS : 4 -6 9 5 -10
EGADS : 5 7 10
EGADS : 6 11 13 -12 -2
EGADS : 7 14 16 -15 -13
EGADS : 8 12 17 -11 -8
EGADS : 9 15 18 -14 -17
EGADS : 10 -16 -18
EGADS : 11 19 20 -21 -22
EGADS : 12 -23 26 25 -24
EGADS : 13 27 23 -28 -19
EGADS : 14 -29 21 30 -25
EGADS : 15 22 29 -26 -27
EGADS : 16 -20 28 24 -30
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes -1 2 3 -4
EGADS : 2 Yes -5 4 6 -7
EGADS : 3 Yes -3 8 1 -9
EGADS : 4 Yes -6 9 5 -10
EGADS : 5 Yes 7 10
EGADS : 6 Yes 11 13 -12 -2
EGADS : 7 Yes 14 16 -15 -13
EGADS : 8 Yes 12 17 -11 -8
EGADS : 9 Yes 15 18 -14 -17
EGADS : 10 Yes -16 -18
EGADS : 11 Yes 19 20 -21 -22
EGADS : 12 Yes -23 26 25 -24
EGADS : 13 Yes 27 23 -28 -19
EGADS : 14 Yes -29 21 30 -25
EGADS : 15 Yes 22 29 -26 -27
EGADS : 16 Yes -20 28 24 -30
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 3 4 1 1 3
EGADS : 4 0 Yes 2 4 1 1 2
EGADS : 5 0 Yes 2 5 1 2 4
EGADS : 6 0 Yes 4 6 1 2 4
EGADS : 7 0 Yes 5 6 1 2 5
EGADS : 8 0 Yes 3 1 1 3 8
EGADS : 9 0 Yes 4 2 1 3 4
EGADS : 10 0 Yes 6 5 1 4 5
EGADS : 11 0 Yes 1 7 1 6 8
EGADS : 12 0 Yes 3 8 1 6 8
EGADS : 13 0 Yes 7 8 1 6 7
EGADS : 14 0 Yes 7 9 1 7 9
EGADS : 15 0 Yes 8 10 1 7 9
EGADS : 16 0 Yes 9 10 1 7 10
EGADS : 17 0 Yes 8 7 1 8 9
EGADS : 18 0 Yes 10 9 1 9 10
EGADS : 19 1 Yes 12 11 NA 11 13
EGADS : 20 1 Yes 11 13 NA 11 16
EGADS : 21 1 Yes 14 13 NA 11 14
EGADS : 22 1 Yes 12 14 NA 11 15
EGADS : 23 1 Yes 16 15 NA 12 13
EGADS : 24 1 Yes 15 17 NA 12 16
EGADS : 25 1 Yes 18 17 NA 12 14
EGADS : 26 1 Yes 16 18 NA 12 15
EGADS : 27 1 Yes 12 16 NA 13 15
EGADS : 28 1 Yes 11 15 NA 13 16
EGADS : 29 1 Yes 14 18 NA 14 15
EGADS : 30 1 Yes 13 17 NA 14 16
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 97.2007855 0 0
EGADS : 2 Yes 97.9335611 0 0
EGADS : 3 Yes 50 0 0
EGADS : 4 Yes 75.3047874 0 0
EGADS : 5 Yes 123.552357 0 4.7180639
EGADS : 6 Yes 118.391317 0 3.99272703
EGADS : 7 Yes 97.9335611 36.1389817 0
EGADS : 8 Yes 75.3047874 36.1389817 0
EGADS : 9 Yes 123.552357 97.6729236 4.7180639
EGADS : 10 Yes 118.391317 97.6729236 3.99272703
EGADS : 11 Yes 0 0 1951.57774
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 1953.45847 1951.57774
EGADS : 14 Yes 0 1953.45847 0
EGADS : 15 Yes 2040.21562 0 1951.57774
EGADS : 16 Yes 2040.21562 0 0
EGADS : 17 Yes 2040.21562 1953.45847 1951.57774
EGADS : 18 Yes 2040.21562 1953.45847 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 3906.92
AFLR4 : Min Bounding Box Length = 3906.92
AFLR4 : Max Ref Bounding Box Length = 195.346
AFLR4 : Min Ref Bounding Box Length = 13.1976
AFLR4 : Reference Length = 13.1976
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 428.309
AFLR4 : Abs Min Surf Spacing = 0.032994
AFLR4 : Min Surf Spacing = 0.065988
AFLR4 : Max Surf Spacing = 1.31976
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 FARFIELD
AFLR4 : 12 CAD geometry 0 FARFIELD
AFLR4 : 13 CAD geometry 0 FARFIELD
AFLR4 : 14 CAD geometry 0 FARFIELD
AFLR4 : 15 CAD geometry 0 FARFIELD
AFLR4 : 16 CAD geometry 0 FARFIELD
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 151708
AFLR43 : Nodes = 75858
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Darwin 22.6.0 x86_64
AFLR3 : Compile Date 11/01/23 @ 12:19PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 75858 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 FarField
UG3 : 12 FarField
UG3 : 13 FarField
UG3 : 14 FarField
UG3 : 15 FarField
UG3 : 16 FarField
AFLR3 : CPU Time = 0.187 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 75858 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 15174 110930
AFLR3 IG : Nodes, Elements = 30348 239495
AFLR3 IG : Nodes, Elements = 45522 364354
AFLR3 IG : Nodes, Elements = 60696 488681
AFLR3 IG : Nodes, Elements = 75865 649510
AFLR3 IG : Nodes, Elements = 75865 648281
AFLR3 IG : Nodes, Elements = 75865 648386
AFLR3 IG : Nodes, Elements = 75865 647473
AFLR3 IG : Nodes, Elements = 75858 416329
AFLR3 IG : Nodes, Elements = 75858 417606
AFLR3 IG : Nodes, Elements = 75858 262264
AFLR3 IG : Nodes, Elements = 75858 239210
AFLR3 : CPU Time = 4.704 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 75858 239210
AFLR3 GG : Nodes, Elements = 97132 303611
AFLR3 GG : Nodes, Elements = 97132 383332
AFLR3 GG : Nodes, Elements = 97132 349683
AFLR3 GG : Nodes, Elements = 114849 406275
AFLR3 GG : Nodes, Elements = 114849 482725
AFLR3 GG : Nodes, Elements = 114849 452697
AFLR3 GG : Nodes, Elements = 138441 525777
AFLR3 GG : Nodes, Elements = 138441 626445
AFLR3 GG : Nodes, Elements = 138441 588368
AFLR3 GG : Nodes, Elements = 163857 666503
AFLR3 GG : Nodes, Elements = 163857 778164
AFLR3 GG : Nodes, Elements = 163857 739558
AFLR3 GG : Nodes, Elements = 192671 827152
AFLR3 GG : Nodes, Elements = 192671 948495
AFLR3 GG : Nodes, Elements = 192671 911626
AFLR3 GG : Nodes, Elements = 222838 1003052
AFLR3 GG : Nodes, Elements = 222838 1125934
AFLR3 GG : Nodes, Elements = 222838 1090493
AFLR3 GG : Nodes, Elements = 253183 1182192
AFLR3 GG : Nodes, Elements = 253183 1304526
AFLR3 GG : Nodes, Elements = 253183 1270346
AFLR3 GG : Nodes, Elements = 282951 1360195
AFLR3 GG : Nodes, Elements = 282951 1479259
AFLR3 GG : Nodes, Elements = 282951 1446989
AFLR3 GG : Nodes, Elements = 311952 1534462
AFLR3 GG : Nodes, Elements = 311952 1650202
AFLR3 GG : Nodes, Elements = 311952 1619110
AFLR3 GG : Nodes, Elements = 340201 1704242
AFLR3 GG : Nodes, Elements = 340201 1816887
AFLR3 GG : Nodes, Elements = 340201 1787199
AFLR3 GG : Nodes, Elements = 367522 1869471
AFLR3 GG : Nodes, Elements = 367522 1977948
AFLR3 GG : Nodes, Elements = 367522 1949599
AFLR3 GG : Nodes, Elements = 393925 2029090
AFLR3 GG : Nodes, Elements = 393925 2132723
AFLR3 GG : Nodes, Elements = 393925 2106488
AFLR3 GG : Nodes, Elements = 419127 2182304
AFLR3 GG : Nodes, Elements = 419127 2282210
AFLR3 GG : Nodes, Elements = 419127 2256356
AFLR3 GG : Nodes, Elements = 443428 2329478
AFLR3 GG : Nodes, Elements = 443428 2424668
AFLR3 GG : Nodes, Elements = 443428 2400581
AFLR3 GG : Nodes, Elements = 466613 2470298
AFLR3 GG : Nodes, Elements = 466613 2561757
AFLR3 GG : Nodes, Elements = 466613 2538297
AFLR3 GG : Nodes, Elements = 488916 2605369
AFLR3 GG : Nodes, Elements = 488916 2692594
AFLR3 GG : Nodes, Elements = 488916 2670787
AFLR3 GG : Nodes, Elements = 509979 2734124
AFLR3 GG : Nodes, Elements = 509979 2817149
AFLR3 GG : Nodes, Elements = 509979 2795823
AFLR3 GG : Nodes, Elements = 530214 2856653
AFLR3 GG : Nodes, Elements = 530214 2935862
AFLR3 GG : Nodes, Elements = 530214 2916089
AFLR3 GG : Nodes, Elements = 549352 2973619
AFLR3 GG : Nodes, Elements = 549352 3048071
AFLR3 GG : Nodes, Elements = 549352 3029658
AFLR3 GG : Nodes, Elements = 567543 3084342
AFLR3 GG : Nodes, Elements = 567543 3155739
AFLR3 GG : Nodes, Elements = 567543 3137536
AFLR3 GG : Nodes, Elements = 584696 3189078
AFLR3 GG : Nodes, Elements = 584696 3256688
AFLR3 GG : Nodes, Elements = 584696 3239442
AFLR3 GG : Nodes, Elements = 600968 3288309
AFLR3 GG : Nodes, Elements = 600968 3352030
AFLR3 GG : Nodes, Elements = 600968 3336020
AFLR3 GG : Nodes, Elements = 616420 3382421
AFLR3 GG : Nodes, Elements = 616420 3443144
AFLR3 GG : Nodes, Elements = 616420 3427558
AFLR3 GG : Nodes, Elements = 630939 3471140
AFLR3 GG : Nodes, Elements = 630939 3527402
AFLR3 GG : Nodes, Elements = 630939 3513502
AFLR3 GG : Nodes, Elements = 644855 3555271
AFLR3 GG : Nodes, Elements = 644855 3609316
AFLR3 GG : Nodes, Elements = 644855 3595966
AFLR3 GG : Nodes, Elements = 657934 3635234
AFLR3 GG : Nodes, Elements = 657934 3686150
AFLR3 GG : Nodes, Elements = 657934 3673508
AFLR3 GG : Nodes, Elements = 670441 3711044
AFLR3 GG : Nodes, Elements = 670441 3760014
AFLR3 GG : Nodes, Elements = 670441 3747555
AFLR3 GG : Nodes, Elements = 682330 3783229
AFLR3 GG : Nodes, Elements = 682330 3829125
AFLR3 GG : Nodes, Elements = 682330 3817950
AFLR3 GG : Nodes, Elements = 693449 3851324
AFLR3 GG : Nodes, Elements = 693449 3895012
AFLR3 GG : Nodes, Elements = 693449 3883830
AFLR3 GG : Nodes, Elements = 704085 3915754
AFLR3 GG : Nodes, Elements = 704085 3957277
AFLR3 GG : Nodes, Elements = 704085 3946774
AFLR3 GG : Nodes, Elements = 714263 3977316
AFLR3 GG : Nodes, Elements = 714263 4017145
AFLR3 GG : Nodes, Elements = 714263 4007033
AFLR3 GG : Nodes, Elements = 723869 4035868
AFLR3 GG : Nodes, Elements = 723869 4073280
AFLR3 GG : Nodes, Elements = 723869 4063890
AFLR3 GG : Nodes, Elements = 733115 4091642
AFLR3 GG : Nodes, Elements = 733115 4127319
AFLR3 GG : Nodes, Elements = 733115 4118494
AFLR3 GG : Nodes, Elements = 741988 4145122
AFLR3 GG : Nodes, Elements = 741988 4179614
AFLR3 GG : Nodes, Elements = 741988 4170907
AFLR3 GG : Nodes, Elements = 750469 4196363
AFLR3 GG : Nodes, Elements = 750469 4229036
AFLR3 GG : Nodes, Elements = 750469 4220990
AFLR3 GG : Nodes, Elements = 758570 4245305
AFLR3 GG : Nodes, Elements = 758570 4276426
AFLR3 GG : Nodes, Elements = 758570 4268815
AFLR3 GG : Nodes, Elements = 766214 4291751
AFLR3 GG : Nodes, Elements = 766214 4321127
AFLR3 GG : Nodes, Elements = 766214 4313899
AFLR3 GG : Nodes, Elements = 773471 4335674
AFLR3 GG : Nodes, Elements = 773471 4363636
AFLR3 GG : Nodes, Elements = 773471 4356867
AFLR3 GG : Nodes, Elements = 780264 4377253
AFLR3 GG : Nodes, Elements = 780264 4403865
AFLR3 GG : Nodes, Elements = 780264 4397085
AFLR3 GG : Nodes, Elements = 786521 4415865
AFLR3 GG : Nodes, Elements = 786521 4440100
AFLR3 GG : Nodes, Elements = 786521 4434150
AFLR3 GG : Nodes, Elements = 792274 4451413
AFLR3 GG : Nodes, Elements = 792274 4473915
AFLR3 GG : Nodes, Elements = 792274 4468098
AFLR3 GG : Nodes, Elements = 797610 4484114
AFLR3 GG : Nodes, Elements = 797610 4504842
AFLR3 GG : Nodes, Elements = 797610 4499716
AFLR3 GG : Nodes, Elements = 802463 4514281
AFLR3 GG : Nodes, Elements = 802463 4533554
AFLR3 GG : Nodes, Elements = 802463 4528446
AFLR3 GG : Nodes, Elements = 806831 4541553
AFLR3 GG : Nodes, Elements = 806831 4558607
AFLR3 GG : Nodes, Elements = 806831 4554331
AFLR3 GG : Nodes, Elements = 810792 4566220
AFLR3 GG : Nodes, Elements = 810792 4581535
AFLR3 GG : Nodes, Elements = 810792 4577663
AFLR3 GG : Nodes, Elements = 814300 4588193
AFLR3 GG : Nodes, Elements = 814300 4602161
AFLR3 GG : Nodes, Elements = 814300 4598395
AFLR3 GG : Nodes, Elements = 817300 4607402
AFLR3 GG : Nodes, Elements = 817300 4619074
AFLR3 GG : Nodes, Elements = 817300 4616093
AFLR3 GG : Nodes, Elements = 819832 4623690
AFLR3 GG : Nodes, Elements = 819832 4633821
AFLR3 GG : Nodes, Elements = 819832 4631104
AFLR3 GG : Nodes, Elements = 821978 4637545
AFLR3 GG : Nodes, Elements = 821978 4645890
AFLR3 GG : Nodes, Elements = 821978 4643791
AFLR3 GG : Nodes, Elements = 823761 4649143
AFLR3 GG : Nodes, Elements = 823761 4656010
AFLR3 GG : Nodes, Elements = 823761 4654216
AFLR3 GG : Nodes, Elements = 825222 4658599
AFLR3 GG : Nodes, Elements = 825222 4664290
AFLR3 GG : Nodes, Elements = 825222 4662855
AFLR3 GG : Nodes, Elements = 826355 4666254
AFLR3 GG : Nodes, Elements = 826355 4670638
AFLR3 GG : Nodes, Elements = 826355 4669496
AFLR3 GG : Nodes, Elements = 827228 4672115
AFLR3 GG : Nodes, Elements = 827228 4675652
AFLR3 GG : Nodes, Elements = 827228 4674674
AFLR3 GG : Nodes, Elements = 827874 4676612
AFLR3 GG : Nodes, Elements = 827874 4679200
AFLR3 GG : Nodes, Elements = 827874 4678461
AFLR3 GG : Nodes, Elements = 828364 4679931
AFLR3 GG : Nodes, Elements = 828364 4681878
AFLR3 GG : Nodes, Elements = 828364 4681343
AFLR3 GG : Nodes, Elements = 828722 4682417
AFLR3 GG : Nodes, Elements = 828722 4683832
AFLR3 GG : Nodes, Elements = 828722 4683437
AFLR3 GG : Nodes, Elements = 828979 4684208
AFLR3 GG : Nodes, Elements = 828979 4685276
AFLR3 GG : Nodes, Elements = 828979 4684962
AFLR3 GG : Nodes, Elements = 829151 4685478
AFLR3 GG : Nodes, Elements = 829151 4686182
AFLR3 GG : Nodes, Elements = 829151 4685989
AFLR3 GG : Nodes, Elements = 829262 4686322
AFLR3 GG : Nodes, Elements = 829262 4686796
AFLR3 GG : Nodes, Elements = 829262 4686629
AFLR3 GG : Nodes, Elements = 829310 4686773
AFLR3 GG : Nodes, Elements = 829310 4686978
AFLR3 GG : Nodes, Elements = 829310 4686908
AFLR3 GG : Nodes, Elements = 829342 4687004
AFLR3 GG : Nodes, Elements = 829342 4687149
AFLR3 GG : Nodes, Elements = 829342 4687098
AFLR3 GG : Nodes, Elements = 829359 4687149
AFLR3 GG : Nodes, Elements = 829359 4687223
AFLR3 GG : Nodes, Elements = 829359 4687197
AFLR3 GG : Nodes, Elements = 829368 4687224
AFLR3 GG : Nodes, Elements = 829368 4687254
AFLR3 GG : Nodes, Elements = 829368 4687245
AFLR3 GG : Nodes, Elements = 829369 4687248
AFLR3 GG : Nodes, Elements = 829369 4687253
AFLR3 GG : Nodes, Elements = 829369 4687252
AFLR3 GG : Nodes, Elements = 829370 4687255
AFLR3 GG : Nodes, Elements = 829370 4687260
AFLR3 GG : Nodes, Elements = 829370 4687255
AFLR3 GG : Nodes, Elements = 829505 4687660
AFLR3 GG : Nodes, Elements = 829505 4688264
AFLR3 GG : Nodes, Elements = 829505 4687976
AFLR3 GG : Nodes, Elements = 829559 4688138
AFLR3 GG : Nodes, Elements = 829559 4688352
AFLR3 GG : Nodes, Elements = 829559 4688272
AFLR3 GG : Nodes, Elements = 829574 4688317
AFLR3 GG : Nodes, Elements = 829574 4688384
AFLR3 GG : Nodes, Elements = 829574 4688356
AFLR3 GG : Nodes, Elements = 829583 4688383
AFLR3 GG : Nodes, Elements = 829583 4688412
AFLR3 GG : Nodes, Elements = 829583 4688405
AFLR3 GG : Nodes, Elements = 829585 4688411
AFLR3 GG : Nodes, Elements = 829585 4688419
AFLR3 GG : Nodes, Elements = 829585 4688416
AFLR3 GG : Nodes, Elements = 829588 4688425
AFLR3 GG : Nodes, Elements = 829588 4688435
AFLR3 GG : Nodes, Elements = 829588 4688432
AFLR3 GG : Nodes, Elements = 829589 4688435
AFLR3 GG : Nodes, Elements = 829589 4688439
AFLR3 GG : Nodes, Elements = 829589 4688438
AFLR3 : CPU Time = 1.605 minutes
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 829589 4688438
AFLR3 QI : Nodes, Elements = 823135 4652250
AFLR3 QI : Nodes, Elements = 821238 4641520
AFLR3 QI : Nodes, Elements = 820685 4638368
AFLR3 QI : Nodes, Elements = 820541 4637549
AFLR3 QI : Nodes, Elements = 820517 4637407
AFLR3 QI : Nodes, Elements = 820510 4637366
AFLR3 QI : Nodes, Elements = 820508 4637355
AFLR3 QI : Nodes, Elements = 820508 4656485
AFLR3 QI : Nodes, Elements = 820508 4634774
AFLR3 QI : Nodes, Elements = 820508 4625695
AFLR3 QI : Nodes, Elements = 820508 4640147
AFLR3 QI : Nodes, Elements = 820508 4625558
AFLR3 QI : Nodes, Elements = 820508 4625078
AFLR3 QI : Nodes, Elements = 820508 4628468
AFLR3 QI : Nodes, Elements = 820508 4623998
AFLR3 QI : Nodes, Elements = 820508 4623361
AFLR3 QI : Nodes, Elements = 820508 4625402
AFLR3 QI : Nodes, Elements = 820508 4623121
AFLR3 QI : Nodes, Elements = 820508 4622741
AFLR3 QI : Nodes, Elements = 820508 4624403
AFLR3 QI : Nodes, Elements = 820508 4622674
AFLR3 QI : Nodes, Elements = 820508 4622390
AFLR3 QI : Nodes, Elements = 820509 4622395
AFLR3 QI : Nodes, Elements = 820509 4623873
AFLR3 QI : Nodes, Elements = 820509 4622388
AFLR3 QI : Nodes, Elements = 820509 4622360
AFLR3 QI : Nodes, Elements = 820509 4623884
AFLR3 QI : Nodes, Elements = 820509 4622359
AFLR3 QI : Nodes, Elements = 820509 4622143
AFLR3 QI : Nodes, Elements = 820509 4622395
AFLR3 : CPU Time = 24.732 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 820509 4622395
AFLR3 QRG: Nodes, Elements = 820508 4622393
AFLR3 : CPU Time = 0.814 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Ang = 6.832 164.7
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 4622393
UG3 : Min Vol = 1.8e-05
UG3 : Average Vol = 1.29e+04
UG3 : Total-Tet-Vol = 5.96e+10
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 = 4622393
UG3 : Min, Max Q = 0.0861 1
UG3 : Average Q = 0.902
UG3 : No. Q< 0.1 = 1
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 2.146 minutes
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Ang = 6.832 164.7
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 2
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 5.96e+10
UG3 : No. Tet Elems = 4622393
UG3 : Min Vol = 1.8e-05
UG3 : Average Vol = 1.29e+04
UG3 : Total-Tet-Vol = 5.96e+10
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 : Note that L includes scaling for BL-aspect=ratio
UG3 : No. Tet Elems = 4622393
UG3 : Min, Max Q = 0.252 1
UG3 : Average Q = 0.862
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.1
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
Volume mesh:
Number of nodes = 820508
Number of elements = 4774101
Number of triangles = 151708
Number of quadrilatarals = 0
Number of tetrahedrals = 4622393
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing
Done getting CFD boundary conditions
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
==> Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Computational Fluid Dynamics Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
Parsing config file for zone 0
----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.294118.
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 4240 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 195.346 m.
Reference origin for moment evaluation is (55.4263, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_1.
Surface(s) plotted in the output file: BC_1.
Surface(s) affected by the design variables: BC_1.
Input mesh file name: ../aflr3/aflr3_CAPS.su2
--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1.
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.
--------------- Time Numerical Integration ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
| MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
| 0| 1| 0| 0|
| 1| 2| 0| 0|
| 2| 3| 0| 0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number: 10
------------------ Convergence Criteria ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 5.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.
-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency:
+------------------------------------+
| File| Frequency|
+------------------------------------+
| RESTART| 250|
| SURFACE_CSV| 250|
| TECPLOT| 250|
| SURFACE_TECPLOT| 250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_aeroelasticIterative.dat.
Surface file name: surface_flow_aeroelasticIterative.
Volume file name: flow_aeroelasticIterative.
Restart file name: restart_flow_aeroelasticIterative.dat.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
-------------------- Output Preprocessing ( Zone 0 ) --------------------
WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE
------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Three dimensional problem.
820508 grid points.
4622393 volume elements.
2 surface markers.
151672 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
4622393 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: 5.96352e+10.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 122.726. Mean K: 4.02926. Standard deviation K: 11.9589.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
| Mesh Quality Metric| Minimum| Maximum|
+--------------------------------------------------------------+
| Orthogonality Angle (deg.)| 45.6095| 87.5269|
| CV Face Area Aspect Ratio| 1.01102| 1685.04|
| CV Sub-Volume Ratio| 1.00273| 21641.9|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
| MG Level| CVs|Aggl. Rate| CFL|
+-------------------------------------------+
| 0| 820508| 1/1.00| 10|
| 1| 134785| 1/6.09| 8.21506|
| 2| 20535| 1/6.56| 6.58142|
+-------------------------------------------+
Finding max control volume width.
Semi-span length = 97.6729 m.
Wetted area = 8795.17 m^2.
Area projection in the x-plane = 681.447 m^2, y-plane = 449.382 m^2, z-plane = 4224.13 m^2.
Max. coordinate in the x-direction = 123.552 m, y-direction = 97.6729 m, z-direction = 4.71806 m.
Min. coordinate in the x-direction = 49.9621 m, y-direction = -97.6729 m, z-direction = -8.47903 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| 211798| 1| m^2/s^2| 211798|
| Velocity-X| 100.087| 1| m/s| 100.087|
| Velocity-Y| 0| 1| m/s| 0|
| Velocity-Z| 0| 1| m/s| 0|
| Velocity Magnitude| 100.087| 1| m/s| 100.087|
+------------------------------------------------------------------------------+
| Mach Number| -| -| -| 0.294118|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.
------------------- Numerics Preprocessing ( Zone 0 ) -------------------
----------------- Integration Preprocessing ( Zone 0 ) ------------------
------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.
------------------------------ Begin Solver -----------------------------
Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
| Time_Iter| Outer_Iter| Inner_Iter| Cur_Time| Time_Step| Time(sec)| rms[Rho]| rms[RhoU]| rms[RhoV]| rms[RhoE]| CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
| 0| 0| 0| 0.0000e+00| 0.0000e+00| 2.2167e+01| 0.145923| 2.266953| 1.873315| 5.615029| -0.743648|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.9975e+01| 3.058492| 5.349987| 5.302922| 8.509821| -0.625296|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.9617e+01| 4.802620| 7.197242| 7.040155| 10.267182| -17.831951|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.9008e+01| 6.552817| 9.201531| 8.840408| 12.012985| -96.832997|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.8717e+01| 6.284338| 8.598720| 8.579102| 11.662845| -3.272926|
----------------------------- Solver Exit -------------------------------
Maximum number of iterations reached (ITER = 5) before convergence.
+-----------------------------------------------------------------------+
| Convergence Field | Value | Criterion | Converged |
+-----------------------------------------------------------------------+
| rms[Rho]| 6.28434| < -14| No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
| File Writing Summary | Filename |
+-----------------------------------------------------------------------+
|SU2 binary restart |restart_flow_aeroelasticIterative.dat|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|CSV file |surface_flow_aeroelasticIterative.csv|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary |flow_aeroelasticIterative.szplt |
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
|Tecplot binary surface |surface_flow_aeroelasticIterative.szplt|
Writing the forces breakdown file (forces_breakdown_aeroelasticIterative.dat).
+-----------------------------------------------------------------------+
Warning: there are 84 non-physical points in the solution.
Warning: 2 reconstructed states for upwinding are non-physical.
--------------------------- Finalizing Solver ---------------------------
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) ------------------------
==> Running SU2 post-analysis...
==> Running ASTROS pre-analysis...
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = wingSpar1, index = 1
Name = wingSpar2, index = 2
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 425
Number of elements = 482
Number of triangle elements = 0
Number of quadrilateral elements = 482
----------------------------
Total number of nodes = 425
Total number of elements = 482
Mapping Csys attributes ................
Number of unique Csys attributes = 2
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Getting FEA coordinate systems.......
Number of coordinate systems - 2
Coordinate system name - leftWingSkin
Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 1
Name = rootConstraint, index = 1
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 4
Name = leftWingSkin, index = 1
Name = riteWingSkin, index = 2
Name = leftPointLoad, index = 3
Name = ritePointLoad, index = 4
Mapping capsBound attributes ................
Number of unique capsBound attributes = 4
Name = upperWing, index = 1
Name = lowerWing, index = 2
Name = leftTip, index = 3
Name = riteTip, index = 4
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsResponse attributes ................
Number of unique capsResponse attributes = 0
Mapping capsReference attributes ................
Number of unique capsReference attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = leftWingSkin, index = 1
Name = wingRib, index = 2
Name = riteWingSkin, index = 3
Name = wingSpar1, index = 4
Name = wingSpar2, index = 5
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 425
Number of elements = 482
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 482
Aero_Reference value is NULL - No aero reference parameters set
Getting FEA materials.......
Number of materials - 2
Material name - Madeupium
Material name - Unobtainium
No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
Done getting FEA materials
Getting FEA properties.......
Number of properties - 5
Property name - leftWingSkin
Property name - riteWingSkin
Property name - wingRib
Property name - wingSpar1
Property name - wingSpar2
Done getting FEA properties
Updating mesh element types based on properties input
Getting FEA constraints.......
Number of constraints - 1
Constraint name - rootConstraint
No "constraintType" specified for Constraint tuple rootConstraint, defaulting to "ZeroDisplacement"
Done getting FEA constraints
Support tuple is NULL - No supports applied
Connect tuple is NULL - Using defaults
Getting FEA loads.......
Number of loads - 1
Load name - pressureAero
No "groupName" specified for Load tuple pressureAero, going to use load name
Done getting FEA loads
Optimization Control tuple is NULL - Default optimization control is used
Getting FEA optimization control.......
Done getting FEA Optimization Control
Design_Variable tuple is NULL - No design variables applied
Design_Constraint tuple is NULL - No design constraints applied
Analysis tuple is NULL
Getting FEA analyses.......
Number of analyses - 1
Analysis name - Default
Done getting FEA analyses
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 75838
CAPS Info: Bound 'upperWing' Normalized Integrated 'Pressure'
Rank 0: src = 3.142010e+12, tgt = 3.142010e+12, diff = 1.288142e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 75838
CAPS Info: Bound 'lowerWing' Normalized Integrated 'Pressure'
Rank 0: src = 3.256490e+12, tgt = 3.256490e+12, diff = 5.826172e+00
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 75838
CAPS Info: Bound 'leftTip' Normalized Integrated 'Pressure'
Rank 0: src = 1.692708e+09, tgt = 1.692706e+09, diff = 1.729559e+03
Reading SU2 AeroLoad File - surface_flow_aeroelasticIterative.csv
Number of variables = 16
Number of data points = 75838
CAPS Info: Bound 'riteTip' Normalized Integrated 'Pressure'
Rank 0: src = 1.250150e+09, tgt = 1.250152e+09, diff = 1.644759e+03
Extracting external pressure loads from data transfer....
TransferName = upperWing
Number of Elements = 98 (total = 98)
Extracting external pressure loads from data transfer....
TransferName = lowerWing
Number of Elements = 98 (total = 196)
Extracting external pressure loads from data transfer....
TransferName = leftTip
Number of Elements = 17 (total = 213)
Extracting external pressure loads from data transfer....
TransferName = riteTip
Number of Elements = 17 (total = 230)
Writing Astros grid and connectivity file (in free field format) ....
Finished writing Astros grid file
Writing subElement types (if any) - appending mesh file
Writing Astros instruction file....
Writing analysis cards
Writing load ADD cards
Writing constraint cards--each subcase individually
Writing load cards
Writing material cards
Writing property cards
Writing coordinate system cards
==> Running mASTROS......
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
==> Running ASTROS post-analysis...
==> Running SU2 pre-analysis...
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
Done boundary flags
Writing SU2 data transfer files
Writing SU2 Motion File - aeroelasticIterative_motion.dat
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
==> Running SU2......
-------------------------------------------------------------------------
| ___ _ _ ___ |
| / __| | | |_ ) Release 8.0.0 "Harrier" |
| \__ \ |_| |/ / |
| |___/\___//___| Suite (Mesh Deformation Code) |
| |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io |
| |
| The SU2 Project is maintained by the SU2 Foundation |
| (http://su2foundation.org) |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors |
| |
| SU2 is free software; you can redistribute it and/or |
| modify it under the terms of the GNU Lesser General Public |
| License as published by the Free Software Foundation; either |
| version 2.1 of the License, or (at your option) any later version. |
| |
| SU2 is distributed in the hope that it will be useful, |
| but WITHOUT ANY WARRANTY; without even the implied warranty of |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU |
| Lesser General Public License for more details. |
| |
| You should have received a copy of the GNU Lesser General Public |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>. |
-------------------------------------------------------------------------
----------------- Physical Case Definition ( Zone 0 ) -------------------
Input mesh file name: ../aflr3/aflr3_CAPS.su2
---------------- Grid deformation parameters ( Zone 0 ) ----------------
Grid deformation using a linear elasticity method.
-------------------- Output Information ( Zone 0 ) ----------------------
Output mesh file name: ../aflr3/aflr3_CAPS.su2.
Cell stiffness scaled by distance to nearest solid surface.
------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
| Marker Type| Marker Name|
+-----------------------------------------------------------------------+
| Euler wall| BC_1|
+-----------------------------------------------------------------------+
| Far-field| BC_2|
+-----------------------------------------------------------------------+
Three dimensional problem.
820508 grid points.
4622393 volume elements.
2 surface markers.
151672 boundary elements in index 0 (Marker = BC_1).
36 boundary elements in index 1 (Marker = BC_2).
4622393 tetrahedra.
----------------------- Preprocessing computations ----------------------
Setting local point connectivity.
Checking the numerical grid orientation of the interior elements.
All volume elements are correctly orientend.
All surface elements are correctly orientend.
Identify edges and vertices.
Setting the bound control volume structure.
Volume of the computational grid: 5.96352e+10.
Info: Ignoring the following volume output fields/groups:
SOLUTION
Volume output fields: COORDINATES
Info: Ignoring the following screen output fields:
RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME
Info: Ignoring the following history output groups:
RMS_RES, AERO_COEFF
History output group(s): ITER, TIME_DOMAIN, WALL_TIME
Warning: No (valid) fields chosen for convergence monitoring. Convergence monitoring inactive.
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
--------------------- Surface grid deformation (ZONE 0) -----------------
Performing the deformation of the surface grid.
Updating the surface coordinates from the input file.
------------------- Volumetric grid deformation (ZONE 0) ----------------
Performing the deformation of the volumetric grid.
Build timed out (after 120 minutes). Marking the build as failed.
Build was aborted
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
SU2 process was terminated by signal '15'
/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/ESP/venv/bin/python: line 8: 60236 Terminated: 15 $PYTHON "$@"
real 129m44.795s
user 55m16.110s
sys 14m51.464s
+ status=143
+ set +x
=================================================
data/session10/2_aeroelastic_Iterative_SU2_Astros.py failed (as NOT expected)
=================================================
/Users/jenkins/workspace/ESP_MemcheckCaps/7.8/CAPS/training/DARWIN64/JenkinsESP/ESP_Sanitize.sh: line 257: 42495 Terminated: 15 bash -e execute_Training.sh
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE
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