Skipping 564 KB..
Full LogAFLR2 : Nodes, Trias,Quads= 158 267 0
AFLR4 : Nodes, Trias,Quads= 145 241 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 67 109 0
AFLR4 : Nodes, Trias,Quads= 45 65 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 26 36 0
AFLR4 : Nodes, Trias,Quads= 20 24 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2793 5566 984
OVERALL : CPU Time = 0.228 seconds
Body 1 (of 5)
Number of nodes = 1595
Number of elements = 3186
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3186
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 301
Number of elements = 598
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 598
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 298
Number of elements = 592
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 592
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 301
Number of elements = 598
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 598
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 298
Number of elements = 592
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 592
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2793
Total number of elements = 5566
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Getting volume mesh for body 1 (of 5)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.1.0 x86_64
AFLR2 : Compile Date 11/20/22 @ 09:24PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Darwin 22.1.0 x86_64
AFLR4 : Compile Date 12/07/22 @ 10:53AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.318 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1595 3186 462
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
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 16.32.36
AFLR3 : Version Date 11/20/22 @ 09:28PM
AFLR3 : Compile OS Darwin 22.1.0 x86_64
AFLR3 : Compile Date 11/20/22 @ 10:24PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 1595 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
AFLR3 : CPU Time = 0.005 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 1595 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 320 1689
AFLR3 IG : Nodes, Elements = 640 3362
AFLR3 IG : Nodes, Elements = 960 4997
AFLR3 IG : Nodes, Elements = 1280 6581
AFLR3 IG : Nodes, Elements = 1600 8125
AFLR3 IG : Nodes, Elements = 1602 8136
AFLR3 IG : Nodes, Elements = 1602 8097
AFLR3 IG : Nodes, Elements = 1595 4634
AFLR3 IG : Nodes, Elements = 1595 4673
AFLR3 IG : Nodes, Elements = 1595 4445
AFLR3 IG : Nodes, Elements = 1595 4438
AFLR3 : CPU Time = 0.026 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 1595 4438
AFLR3 GG : Nodes, Elements = 1920 5413
AFLR3 GG : Nodes, Elements = 1920 6730
AFLR3 GG : Nodes, Elements = 1920 6359
AFLR3 GG : Nodes, Elements = 2094 6881
AFLR3 GG : Nodes, Elements = 2094 7705
AFLR3 GG : Nodes, Elements = 2094 7426
AFLR3 GG : Nodes, Elements = 2148 7588
AFLR3 GG : Nodes, Elements = 2148 7831
AFLR3 GG : Nodes, Elements = 2148 7749
AFLR3 GG : Nodes, Elements = 2160 7785
AFLR3 GG : Nodes, Elements = 2160 7829
AFLR3 GG : Nodes, Elements = 2160 7816
AFLR3 GG : Nodes, Elements = 2162 7822
AFLR3 GG : Nodes, Elements = 2162 7826
AFLR3 : CPU Time = 0.020 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 2162 7826
AFLR3 QI : Nodes, Elements = 2161 7821
AFLR3 QI : Nodes, Elements = 2161 7853
AFLR3 QI : Nodes, Elements = 2161 7820
AFLR3 QI : Nodes, Elements = 2161 7795
AFLR3 QI : Nodes, Elements = 2161 7799
AFLR3 QI : Nodes, Elements = 2161 7792
AFLR3 QI : Nodes, Elements = 2161 7791
AFLR3 : CPU Time = 0.008 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 7791
UG3 : Min, Max Ang = 20.17 146.6
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.1
UG3 : No. Tet Elems = 7791
UG3 : Min Vol = 1.27e-06
UG3 : Average Vol = 1.28e-05
UG3 : Total-Tet-Vol = 0.1
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 = 7791
UG3 : Min, Max Q = 0.508 0.999
UG3 : Average Q = 0.86
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 7791
UG3 : Min, Max Ang = 20.17 146.6
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.1
UG3 : No. Tet Elems = 7791
UG3 : Min Vol = 1.27e-06
UG3 : Average Vol = 1.28e-05
UG3 : Total-Tet-Vol = 0.1
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 = 7791
UG3 : Min, Max Q = 0.522 1
UG3 : Average Q = 0.86
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.282 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.021 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 301 598 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 301 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 301 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 338
AFLR3 IG : Nodes, Elements = 124 736
AFLR3 IG : Nodes, Elements = 186 1135
AFLR3 IG : Nodes, Elements = 248 1546
AFLR3 IG : Nodes, Elements = 308 1953
AFLR3 IG : Nodes, Elements = 301 1093
AFLR3 IG : Nodes, Elements = 301 941
AFLR3 IG : Nodes, Elements = 301 829
AFLR3 : CPU Time = 0.004 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 301 829
AFLR3 GG : Nodes, Elements = 349 973
AFLR3 GG : Nodes, Elements = 349 1076
AFLR3 GG : Nodes, Elements = 349 1030
AFLR3 GG : Nodes, Elements = 382 1129
AFLR3 GG : Nodes, Elements = 382 1292
AFLR3 GG : Nodes, Elements = 382 1245
AFLR3 GG : Nodes, Elements = 399 1296
AFLR3 GG : Nodes, Elements = 399 1370
AFLR3 GG : Nodes, Elements = 399 1349
AFLR3 GG : Nodes, Elements = 408 1376
AFLR3 GG : Nodes, Elements = 408 1409
AFLR3 GG : Nodes, Elements = 408 1393
AFLR3 GG : Nodes, Elements = 411 1402
AFLR3 GG : Nodes, Elements = 411 1411
AFLR3 GG : Nodes, Elements = 411 1410
AFLR3 : CPU Time = 0.005 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 411 1410
AFLR3 QI : Nodes, Elements = 411 1425
AFLR3 QI : Nodes, Elements = 411 1412
AFLR3 QI : Nodes, Elements = 411 1410
AFLR3 QI : Nodes, Elements = 411 1411
AFLR3 QI : Nodes, Elements = 411 1409
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1409
UG3 : Min, Max Ang = 19.95 147.8
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1409
UG3 : Min Vol = 1.17e-06
UG3 : Average Vol = 1.3e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1409
UG3 : Min, Max Q = 0.497 0.997
UG3 : Average Q = 0.86
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1409
UG3 : Min, Max Ang = 19.95 147.8
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1409
UG3 : Min Vol = 1.17e-06
UG3 : Average Vol = 1.3e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1409
UG3 : Min, Max Q = 0.556 1
UG3 : Average Q = 0.87
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.023 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.019 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 298 592 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 298 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 298 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 343
AFLR3 IG : Nodes, Elements = 124 749
AFLR3 IG : Nodes, Elements = 186 1146
AFLR3 IG : Nodes, Elements = 248 1560
AFLR3 IG : Nodes, Elements = 305 1937
AFLR3 IG : Nodes, Elements = 298 1080
AFLR3 IG : Nodes, Elements = 298 937
AFLR3 IG : Nodes, Elements = 298 819
AFLR3 : CPU Time = 0.005 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 298 819
AFLR3 GG : Nodes, Elements = 342 951
AFLR3 GG : Nodes, Elements = 342 1044
AFLR3 GG : Nodes, Elements = 342 983
AFLR3 GG : Nodes, Elements = 376 1085
AFLR3 GG : Nodes, Elements = 376 1256
AFLR3 GG : Nodes, Elements = 376 1209
AFLR3 GG : Nodes, Elements = 395 1266
AFLR3 GG : Nodes, Elements = 395 1349
AFLR3 GG : Nodes, Elements = 395 1321
AFLR3 GG : Nodes, Elements = 401 1339
AFLR3 GG : Nodes, Elements = 401 1364
AFLR3 GG : Nodes, Elements = 401 1352
AFLR3 GG : Nodes, Elements = 403 1358
AFLR3 GG : Nodes, Elements = 403 1368
AFLR3 GG : Nodes, Elements = 403 1363
AFLR3 GG : Nodes, Elements = 405 1369
AFLR3 GG : Nodes, Elements = 405 1377
AFLR3 GG : Nodes, Elements = 405 1374
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 405 1374
AFLR3 QI : Nodes, Elements = 405 1381
AFLR3 QI : Nodes, Elements = 405 1375
AFLR3 QI : Nodes, Elements = 405 1372
AFLR3 QI : Nodes, Elements = 405 1376
AFLR3 QI : Nodes, Elements = 405 1369
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1369
UG3 : Min, Max Ang = 21.02 132.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1369
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.34e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1369
UG3 : Min, Max Q = 0.578 0.999
UG3 : Average Q = 0.858
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1369
UG3 : Min, Max Ang = 21.02 132.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1369
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.34e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1369
UG3 : Min, Max Q = 0.661 1
UG3 : Average Q = 0.873
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.019 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.019 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 301 598 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 301 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 301 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 337
AFLR3 IG : Nodes, Elements = 124 738
AFLR3 IG : Nodes, Elements = 186 1163
AFLR3 IG : Nodes, Elements = 248 1543
AFLR3 IG : Nodes, Elements = 308 1980
AFLR3 IG : Nodes, Elements = 301 1112
AFLR3 IG : Nodes, Elements = 301 972
AFLR3 IG : Nodes, Elements = 301 823
AFLR3 : CPU Time = 0.004 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 301 823
AFLR3 GG : Nodes, Elements = 354 982
AFLR3 GG : Nodes, Elements = 354 1132
AFLR3 GG : Nodes, Elements = 354 1056
AFLR3 GG : Nodes, Elements = 382 1140
AFLR3 GG : Nodes, Elements = 382 1293
AFLR3 GG : Nodes, Elements = 382 1237
AFLR3 GG : Nodes, Elements = 399 1288
AFLR3 GG : Nodes, Elements = 399 1362
AFLR3 GG : Nodes, Elements = 399 1336
AFLR3 GG : Nodes, Elements = 405 1354
AFLR3 GG : Nodes, Elements = 405 1386
AFLR3 GG : Nodes, Elements = 405 1370
AFLR3 GG : Nodes, Elements = 410 1385
AFLR3 GG : Nodes, Elements = 410 1399
AFLR3 GG : Nodes, Elements = 410 1398
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 410 1398
AFLR3 QI : Nodes, Elements = 410 1405
AFLR3 QI : Nodes, Elements = 410 1398
AFLR3 QI : Nodes, Elements = 410 1393
AFLR3 QI : Nodes, Elements = 410 1394
AFLR3 QI : Nodes, Elements = 410 1392
AFLR3 : CPU Time = 0.001 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1392
UG3 : Min, Max Ang = 13.52 154.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1392
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.32e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1392
UG3 : Min, Max Q = 0.419 0.998
UG3 : Average Q = 0.863
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1392
UG3 : Min, Max Ang = 13.52 154.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1392
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.32e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1392
UG3 : Min, Max Q = 0.495 1
UG3 : Average Q = 0.88
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.021 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.021 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 298 592 132
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 298 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 298 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 334
AFLR3 IG : Nodes, Elements = 124 726
AFLR3 IG : Nodes, Elements = 186 1151
AFLR3 IG : Nodes, Elements = 248 1547
AFLR3 IG : Nodes, Elements = 305 1919
AFLR3 IG : Nodes, Elements = 298 1076
AFLR3 IG : Nodes, Elements = 298 931
AFLR3 IG : Nodes, Elements = 298 822
AFLR3 : CPU Time = 0.005 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 298 822
AFLR3 GG : Nodes, Elements = 349 975
AFLR3 GG : Nodes, Elements = 349 1115
AFLR3 GG : Nodes, Elements = 349 1047
AFLR3 GG : Nodes, Elements = 383 1149
AFLR3 GG : Nodes, Elements = 383 1311
AFLR3 GG : Nodes, Elements = 383 1254
AFLR3 GG : Nodes, Elements = 399 1302
AFLR3 GG : Nodes, Elements = 399 1374
AFLR3 GG : Nodes, Elements = 399 1350
AFLR3 GG : Nodes, Elements = 403 1362
AFLR3 GG : Nodes, Elements = 403 1377
AFLR3 GG : Nodes, Elements = 403 1376
AFLR3 : CPU Time = 0.003 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 403 1376
AFLR3 QI : Nodes, Elements = 402 1370
AFLR3 QI : Nodes, Elements = 402 1376
AFLR3 QI : Nodes, Elements = 402 1371
AFLR3 QI : Nodes, Elements = 402 1365
AFLR3 QI : Nodes, Elements = 402 1368
AFLR3 QI : Nodes, Elements = 402 1364
AFLR3 QI : Nodes, Elements = 402 1363
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1363
UG3 : Min, Max Ang = 21.47 133.3
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1363
UG3 : Min Vol = 1.71e-06
UG3 : Average Vol = 1.35e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1363
UG3 : Min, Max Q = 0.599 0.999
UG3 : Average Q = 0.859
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1363
UG3 : Min, Max Ang = 21.47 133.3
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1363
UG3 : Min Vol = 1.71e-06
UG3 : Average Vol = 1.35e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1363
UG3 : Min, Max Q = 0.649 1
UG3 : Average Q = 0.878
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.023 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Volume mesh:
Number of nodes = 3789
Number of elements = 18890
Number of triangles = 5566
Number of quadrilatarals = 0
Number of tetrahedrals = 13324
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing VTK file: volume.vtk....
Finished writing VTK file
Writing exodus file ....
Block: 'tableTop', blk_id 1, num_entries 7791
Block: 'leg0', blk_id 2, num_entries 1409
Block: 'leg1', blk_id 3, num_entries 1369
Block: 'leg2', blk_id 4, num_entries 1392
Block: 'leg3', blk_id 5, num_entries 1363
Sideset: 'leg0Side', set_id 1, num_entries 598
Sideset: 'leg1Side', set_id 2, num_entries 592
Sideset: 'leg2Side', set_id 3, num_entries 598
Sideset: 'leg3Side', set_id 4, num_entries 592
Sideset: 'tableTopSide', set_id 5, num_entries 3186
Nodeset: 'edge', set_id 1, num_entries 25
Nodeset: 'face1', set_id 2, num_entries 244
Nodeset: 'face2', set_id 3, num_entries 248
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
real 0m2.777s
user 0m2.203s
sys 0m0.440s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_aflr_table_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_aflr_table_morph_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
plato_aflr_table_morph_PyTest.py test;
+ python -u plato_aflr_table_morph_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.1.0 x86_64
AFLR2 : Compile Date 11/20/22 @ 09:24PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Darwin 22.1.0 x86_64
AFLR4 : Compile Date 12/07/22 @ 10:53AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 5 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 6 Faces
EGADS : Body 0 has 12 Edges
EGADS : Body 0 has 6 Loops
EGADS : Body 0 has 8 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 6 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 4 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 4 Loops
EGADS : Body 2 has 4 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 4 Faces
EGADS : Body 3 has 6 Edges
EGADS : Body 3 has 4 Loops
EGADS : Body 3 has 4 Nodes
EGADS : Body 4 is a SolidBody
EGADS : Body 4 has 1 Shells
EGADS : Body 4 has 4 Faces
EGADS : Body 4 has 6 Edges
EGADS : Body 4 has 4 Loops
EGADS : Body 4 has 4 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 0 1 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 3 4 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 5 6
EGADS : 4 Yes 0 0 1 0 1 1 2 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 3 4
EGADS : 6 Yes 0 0 1 0 1 1 2 3 4
EGADS : 7 Yes 1 0 1 0 1 8 9 10
EGADS : 8 Yes 1 0 1 0 1 7 9 10
EGADS : 9 Yes 1 0 1 0 1 7 8
EGADS : 10 Yes 1 0 1 0 1 7 8
EGADS : 11 Yes 2 0 1 0 1 12 13 14
EGADS : 12 Yes 2 0 1 0 1 11 13 14
EGADS : 13 Yes 2 0 1 0 1 11 12
EGADS : 14 Yes 2 0 1 0 1 11 12
EGADS : 15 Yes 3 0 1 0 1 16 17 18
EGADS : 16 Yes 3 0 1 0 1 15 17 18
EGADS : 17 Yes 3 0 1 0 1 15 16
EGADS : 18 Yes 3 0 1 0 1 15 16
EGADS : 19 Yes 4 0 1 0 1 20 21 22
EGADS : 20 Yes 4 0 1 0 1 19 21 22
EGADS : 21 Yes 4 0 1 0 1 19 20
EGADS : 22 Yes 4 0 1 0 1 19 20
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 -5 8 7 -6
EGADS : 3 9 5 -10 -1
EGADS : 4 -11 3 12 -7
EGADS : 5 4 11 -8 -9
EGADS : 6 -2 10 6 -12
EGADS : 7 -13 -14 15 16
EGADS : 8 17 14 -18 -16
EGADS : 9 13 18
EGADS : 10 -15 -17
EGADS : 11 -19 -20 21 22
EGADS : 12 23 20 -24 -22
EGADS : 13 19 24
EGADS : 14 -21 -23
EGADS : 15 -25 -26 27 28
EGADS : 16 29 26 -30 -28
EGADS : 17 25 30
EGADS : 18 -27 -29
EGADS : 19 -31 -32 33 34
EGADS : 20 35 32 -36 -34
EGADS : 21 31 36
EGADS : 22 -33 -35
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 : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 -5 8 7 -6
EGADS : 3 Yes 1 9 5 -10 -1
EGADS : 4 Yes 1 -11 3 12 -7
EGADS : 5 Yes 1 4 11 -8 -9
EGADS : 6 Yes 1 -2 10 6 -12
EGADS : 7 Yes 1 -13 -14 15 16
EGADS : 8 Yes 1 17 14 -18 -16
EGADS : 9 Yes 1 13 18
EGADS : 10 Yes 1 -15 -17
EGADS : 11 Yes 1 -19 -20 21 22
EGADS : 12 Yes 1 23 20 -24 -22
EGADS : 13 Yes 1 19 24
EGADS : 14 Yes 1 -21 -23
EGADS : 15 Yes 1 -25 -26 27 28
EGADS : 16 Yes 1 29 26 -30 -28
EGADS : 17 Yes 1 25 30
EGADS : 18 Yes 1 -27 -29
EGADS : 19 Yes 1 -31 -32 33 34
EGADS : 20 Yes 1 35 32 -36 -34
EGADS : 21 Yes 1 31 36
EGADS : 22 Yes 1 -33 -35
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 2 1 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 6 5 1 2 3
EGADS : 6 0 Yes 5 7 1 2 6
EGADS : 7 0 Yes 8 7 1 2 4
EGADS : 8 0 Yes 6 8 1 2 5
EGADS : 9 0 Yes 2 6 1 3 5
EGADS : 10 0 Yes 1 5 1 3 6
EGADS : 11 0 Yes 4 8 1 4 5
EGADS : 12 0 Yes 3 7 1 4 6
EGADS : 13 1 Yes 10 9 1 7 9
EGADS : 14 1 Yes 11 10 1 7 8
EGADS : 15 1 Yes 11 12 1 7 10
EGADS : 16 1 Yes 12 9 1 7 8
EGADS : 17 1 Yes 12 11 1 8 10
EGADS : 18 1 Yes 9 10 1 8 9
EGADS : 19 2 Yes 14 13 1 11 13
EGADS : 20 2 Yes 15 14 1 11 12
EGADS : 21 2 Yes 15 16 1 11 14
EGADS : 22 2 Yes 16 13 1 11 12
EGADS : 23 2 Yes 16 15 1 12 14
EGADS : 24 2 Yes 13 14 1 12 13
EGADS : 25 3 Yes 18 17 1 15 17
EGADS : 26 3 Yes 19 18 1 15 16
EGADS : 27 3 Yes 19 20 1 15 18
EGADS : 28 3 Yes 20 17 1 15 16
EGADS : 29 3 Yes 20 19 1 16 18
EGADS : 30 3 Yes 17 18 1 16 17
EGADS : 31 4 Yes 22 21 1 19 21
EGADS : 32 4 Yes 23 22 1 19 20
EGADS : 33 4 Yes 23 24 1 19 22
EGADS : 34 4 Yes 24 21 1 19 20
EGADS : 35 4 Yes 24 23 1 20 22
EGADS : 36 4 Yes 21 22 1 20 21
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0.5
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 0.1 0.5
EGADS : 4 Yes 0 0.1 0
EGADS : 5 Yes 0.5 0 0.5
EGADS : 6 Yes 0.5 0 0
EGADS : 7 Yes 0.5 0.1 0.5
EGADS : 8 Yes 0.5 0.1 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 0 0 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 0 0.26
EGADS : 14 Yes 0 0 0.46
EGADS : 15 Yes 0 0 0.46
EGADS : 16 Yes 0 0 0.26
EGADS : 17 Yes 0.36 0 0.26
EGADS : 18 Yes 0.36 0 0.46
EGADS : 19 Yes 0.36 0 0.46
EGADS : 20 Yes 0.36 0 0.26
EGADS : 21 Yes 0.36 0 0
EGADS : 22 Yes 0.36 0 0
EGADS : 23 Yes 0.36 0 0
EGADS : 24 Yes 0.36 0 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 1
AFLR4 : Min Bounding Box Length = 0.7
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 0.7
AFLR4 : Reference Length = 10
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.025
AFLR4 : Min Surf Spacing = 0.05
AFLR4 : Max Surf Spacing = 1
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 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 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : Case has 5 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6
AFLR4 : Component 2 includes Definitions 7 8 9 10
AFLR4 : Component 3 includes Definitions 11 12 13 14
AFLR4 : Component 4 includes Definitions 15 16 17 18
AFLR4 : Component 5 includes Definitions 19 20 21 22
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 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 12 14 0
AFLR4 : Nodes, Trias,Quads= 8 6 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 9 10 0
AFLR4 : Nodes, Trias,Quads= 6 4 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 30 42 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 31 44 0
AFLR4 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 30 42 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 31 44 0
AFLR4 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 30 42 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 31 44 0
AFLR4 : Nodes, Trias,Quads= 23 28 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 118 194 0
AFLR4 : Nodes, Trias,Quads= 117 192 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 30 42 0
AFLR4 : Nodes, Trias,Quads= 22 26 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 31 44 0
AFLR4 : Nodes, Trias,Quads= 23 28 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 900 1780 488
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Trias = 900 1780
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Nodes, Trias,Quads= 11 10 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 15 18 0
AFLR4 : Nodes, Trias,Quads= 11 10 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 11 13 0
AFLR4 : Nodes, Trias,Quads= 7 5 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 126 210 0
AFLR4 : Nodes, Trias,Quads= 120 198 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 25 34 0
AFLR4 : Nodes, Trias,Quads= 21 26 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 926 1832 480
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 986 1952
AFLR4 : Nodes, Trias = 1206 2392
AFLR4 : Nodes, Trias = 1760 3500
AFLR4 : Nodes, Trias = 2067 4114
AFLR4 : Nodes, Trias = 2106 4192
AFLR4 : Nodes, Trias = 2108 4196
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 110 160 0
AFLR4 : Nodes, Trias,Quads= 120 180 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 119 175 0
AFLR4 : Nodes, Trias,Quads= 126 189 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 992 1859 0
AFLR4 : Nodes, Trias,Quads= 706 1287 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 625 1152 0
AFLR4 : Nodes, Trias,Quads= 618 1138 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 115 167 0
AFLR4 : Nodes, Trias,Quads= 128 193 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 127 189 0
AFLR4 : Nodes, Trias,Quads= 132 199 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 155 262 0
AFLR4 : Nodes, Trias,Quads= 145 242 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 165 280 0
AFLR4 : Nodes, Trias,Quads= 156 262 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 62 100 0
AFLR4 : Nodes, Trias,Quads= 47 70 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 26 36 0
AFLR4 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 154 260 0
AFLR4 : Nodes, Trias,Quads= 144 240 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 168 286 0
AFLR4 : Nodes, Trias,Quads= 154 258 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 63 102 0
AFLR4 : Nodes, Trias,Quads= 47 70 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 26 36 0
AFLR4 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 163 276 0
AFLR4 : Nodes, Trias,Quads= 156 262 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 155 262 0
AFLR4 : Nodes, Trias,Quads= 145 242 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 63 102 0
AFLR4 : Nodes, Trias,Quads= 47 70 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 26 36 0
AFLR4 : Nodes, Trias,Quads= 20 24 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 166 282 0
AFLR4 : Nodes, Trias,Quads= 156 262 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 158 267 0
AFLR4 : Nodes, Trias,Quads= 145 241 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 67 109 0
AFLR4 : Nodes, Trias,Quads= 45 65 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 26 36 0
AFLR4 : Nodes, Trias,Quads= 20 24 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 2793 5566 984
OVERALL : CPU Time = 0.208 seconds
Body 1 (of 5)
Number of nodes = 1595
Number of elements = 3186
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3186
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 301
Number of elements = 598
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 598
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 298
Number of elements = 592
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 592
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 301
Number of elements = 598
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 598
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 298
Number of elements = 592
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 592
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2793
Total number of elements = 5566
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Getting volume mesh for body 1 (of 5)
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.1.0 x86_64
AFLR2 : Compile Date 11/20/22 @ 09:24PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Darwin 22.1.0 x86_64
AFLR4 : Compile Date 12/07/22 @ 10:53AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.298 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 1595 3186 462
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
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 16.32.36
AFLR3 : Version Date 11/20/22 @ 09:28PM
AFLR3 : Compile OS Darwin 22.1.0 x86_64
AFLR3 : Compile Date 11/20/22 @ 10:24PM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 1595 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
AFLR3 : CPU Time = 0.004 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 1595 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 320 1689
AFLR3 IG : Nodes, Elements = 640 3362
AFLR3 IG : Nodes, Elements = 960 4997
AFLR3 IG : Nodes, Elements = 1280 6581
AFLR3 IG : Nodes, Elements = 1600 8125
AFLR3 IG : Nodes, Elements = 1602 8136
AFLR3 IG : Nodes, Elements = 1602 8097
AFLR3 IG : Nodes, Elements = 1595 4634
AFLR3 IG : Nodes, Elements = 1595 4673
AFLR3 IG : Nodes, Elements = 1595 4445
AFLR3 IG : Nodes, Elements = 1595 4438
AFLR3 : CPU Time = 0.021 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 1595 4438
AFLR3 GG : Nodes, Elements = 1920 5413
AFLR3 GG : Nodes, Elements = 1920 6730
AFLR3 GG : Nodes, Elements = 1920 6359
AFLR3 GG : Nodes, Elements = 2094 6881
AFLR3 GG : Nodes, Elements = 2094 7705
AFLR3 GG : Nodes, Elements = 2094 7426
AFLR3 GG : Nodes, Elements = 2148 7588
AFLR3 GG : Nodes, Elements = 2148 7831
AFLR3 GG : Nodes, Elements = 2148 7749
AFLR3 GG : Nodes, Elements = 2160 7785
AFLR3 GG : Nodes, Elements = 2160 7829
AFLR3 GG : Nodes, Elements = 2160 7816
AFLR3 GG : Nodes, Elements = 2162 7822
AFLR3 GG : Nodes, Elements = 2162 7826
AFLR3 : CPU Time = 0.023 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 2162 7826
AFLR3 QI : Nodes, Elements = 2161 7821
AFLR3 QI : Nodes, Elements = 2161 7853
AFLR3 QI : Nodes, Elements = 2161 7820
AFLR3 QI : Nodes, Elements = 2161 7795
AFLR3 QI : Nodes, Elements = 2161 7799
AFLR3 QI : Nodes, Elements = 2161 7792
AFLR3 QI : Nodes, Elements = 2161 7791
AFLR3 : CPU Time = 0.011 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 7791
UG3 : Min, Max Ang = 20.17 146.6
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.1
UG3 : No. Tet Elems = 7791
UG3 : Min Vol = 1.27e-06
UG3 : Average Vol = 1.28e-05
UG3 : Total-Tet-Vol = 0.1
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 = 7791
UG3 : Min, Max Q = 0.508 0.999
UG3 : Average Q = 0.86
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 7791
UG3 : Min, Max Ang = 20.17 146.6
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.1
UG3 : No. Tet Elems = 7791
UG3 : Min Vol = 1.27e-06
UG3 : Average Vol = 1.28e-05
UG3 : Total-Tet-Vol = 0.1
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 = 7791
UG3 : Min, Max Q = 0.522 1
UG3 : Average Q = 0.86
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.338 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.024 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 301 598 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 301 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 301 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 338
AFLR3 IG : Nodes, Elements = 124 736
AFLR3 IG : Nodes, Elements = 186 1135
AFLR3 IG : Nodes, Elements = 248 1546
AFLR3 IG : Nodes, Elements = 308 1953
AFLR3 IG : Nodes, Elements = 301 1093
AFLR3 IG : Nodes, Elements = 301 941
AFLR3 IG : Nodes, Elements = 301 829
AFLR3 : CPU Time = 0.005 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 301 829
AFLR3 GG : Nodes, Elements = 349 973
AFLR3 GG : Nodes, Elements = 349 1076
AFLR3 GG : Nodes, Elements = 349 1030
AFLR3 GG : Nodes, Elements = 382 1129
AFLR3 GG : Nodes, Elements = 382 1292
AFLR3 GG : Nodes, Elements = 382 1245
AFLR3 GG : Nodes, Elements = 399 1296
AFLR3 GG : Nodes, Elements = 399 1370
AFLR3 GG : Nodes, Elements = 399 1349
AFLR3 GG : Nodes, Elements = 408 1376
AFLR3 GG : Nodes, Elements = 408 1409
AFLR3 GG : Nodes, Elements = 408 1393
AFLR3 GG : Nodes, Elements = 411 1402
AFLR3 GG : Nodes, Elements = 411 1411
AFLR3 GG : Nodes, Elements = 411 1410
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 411 1410
AFLR3 QI : Nodes, Elements = 411 1425
AFLR3 QI : Nodes, Elements = 411 1412
AFLR3 QI : Nodes, Elements = 411 1410
AFLR3 QI : Nodes, Elements = 411 1411
AFLR3 QI : Nodes, Elements = 411 1409
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1409
UG3 : Min, Max Ang = 19.95 147.8
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1409
UG3 : Min Vol = 1.17e-06
UG3 : Average Vol = 1.3e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1409
UG3 : Min, Max Q = 0.497 0.997
UG3 : Average Q = 0.86
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1409
UG3 : Min, Max Ang = 19.95 147.8
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1409
UG3 : Min Vol = 1.17e-06
UG3 : Average Vol = 1.3e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1409
UG3 : Min, Max Q = 0.556 1
UG3 : Average Q = 0.87
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.020 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.021 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 298 592 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 298 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 298 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 343
AFLR3 IG : Nodes, Elements = 124 749
AFLR3 IG : Nodes, Elements = 186 1146
AFLR3 IG : Nodes, Elements = 248 1560
AFLR3 IG : Nodes, Elements = 305 1937
AFLR3 IG : Nodes, Elements = 298 1080
AFLR3 IG : Nodes, Elements = 298 937
AFLR3 IG : Nodes, Elements = 298 819
AFLR3 : CPU Time = 0.006 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 298 819
AFLR3 GG : Nodes, Elements = 342 951
AFLR3 GG : Nodes, Elements = 342 1044
AFLR3 GG : Nodes, Elements = 342 983
AFLR3 GG : Nodes, Elements = 376 1085
AFLR3 GG : Nodes, Elements = 376 1256
AFLR3 GG : Nodes, Elements = 376 1209
AFLR3 GG : Nodes, Elements = 395 1266
AFLR3 GG : Nodes, Elements = 395 1349
AFLR3 GG : Nodes, Elements = 395 1321
AFLR3 GG : Nodes, Elements = 401 1339
AFLR3 GG : Nodes, Elements = 401 1364
AFLR3 GG : Nodes, Elements = 401 1352
AFLR3 GG : Nodes, Elements = 403 1358
AFLR3 GG : Nodes, Elements = 403 1368
AFLR3 GG : Nodes, Elements = 403 1363
AFLR3 GG : Nodes, Elements = 405 1369
AFLR3 GG : Nodes, Elements = 405 1377
AFLR3 GG : Nodes, Elements = 405 1374
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 405 1374
AFLR3 QI : Nodes, Elements = 405 1381
AFLR3 QI : Nodes, Elements = 405 1375
AFLR3 QI : Nodes, Elements = 405 1372
AFLR3 QI : Nodes, Elements = 405 1376
AFLR3 QI : Nodes, Elements = 405 1369
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1369
UG3 : Min, Max Ang = 21.02 132.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1369
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.34e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1369
UG3 : Min, Max Q = 0.578 0.999
UG3 : Average Q = 0.858
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1369
UG3 : Min, Max Ang = 21.02 132.9
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1369
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.34e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1369
UG3 : Min, Max Q = 0.661 1
UG3 : Average Q = 0.873
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.024 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.022 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 301 598 130
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 301 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 301 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 337
AFLR3 IG : Nodes, Elements = 124 738
AFLR3 IG : Nodes, Elements = 186 1163
AFLR3 IG : Nodes, Elements = 248 1543
AFLR3 IG : Nodes, Elements = 308 1980
AFLR3 IG : Nodes, Elements = 301 1112
AFLR3 IG : Nodes, Elements = 301 972
AFLR3 IG : Nodes, Elements = 301 823
AFLR3 : CPU Time = 0.004 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 301 823
AFLR3 GG : Nodes, Elements = 354 982
AFLR3 GG : Nodes, Elements = 354 1132
AFLR3 GG : Nodes, Elements = 354 1056
AFLR3 GG : Nodes, Elements = 382 1140
AFLR3 GG : Nodes, Elements = 382 1293
AFLR3 GG : Nodes, Elements = 382 1237
AFLR3 GG : Nodes, Elements = 399 1288
AFLR3 GG : Nodes, Elements = 399 1362
AFLR3 GG : Nodes, Elements = 399 1336
AFLR3 GG : Nodes, Elements = 405 1354
AFLR3 GG : Nodes, Elements = 405 1386
AFLR3 GG : Nodes, Elements = 405 1370
AFLR3 GG : Nodes, Elements = 410 1385
AFLR3 GG : Nodes, Elements = 410 1399
AFLR3 GG : Nodes, Elements = 410 1398
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 410 1398
AFLR3 QI : Nodes, Elements = 410 1405
AFLR3 QI : Nodes, Elements = 410 1398
AFLR3 QI : Nodes, Elements = 410 1393
AFLR3 QI : Nodes, Elements = 410 1394
AFLR3 QI : Nodes, Elements = 410 1392
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1392
UG3 : Min, Max Ang = 13.52 154.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1392
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.32e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1392
UG3 : Min, Max Q = 0.419 0.998
UG3 : Average Q = 0.863
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1392
UG3 : Min, Max Ang = 13.52 154.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1392
UG3 : Min Vol = 1.15e-06
UG3 : Average Vol = 1.32e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1392
UG3 : Min, Max Q = 0.495 1
UG3 : Average Q = 0.88
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.020 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.019 seconds
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 298 592 132
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 298 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
AFLR3 : CPU Time = 0.001 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 298 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 62 334
AFLR3 IG : Nodes, Elements = 124 726
AFLR3 IG : Nodes, Elements = 186 1151
AFLR3 IG : Nodes, Elements = 248 1547
AFLR3 IG : Nodes, Elements = 305 1919
AFLR3 IG : Nodes, Elements = 298 1076
AFLR3 IG : Nodes, Elements = 298 931
AFLR3 IG : Nodes, Elements = 298 822
AFLR3 : CPU Time = 0.005 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 298 822
AFLR3 GG : Nodes, Elements = 349 975
AFLR3 GG : Nodes, Elements = 349 1115
AFLR3 GG : Nodes, Elements = 349 1047
AFLR3 GG : Nodes, Elements = 383 1149
AFLR3 GG : Nodes, Elements = 383 1311
AFLR3 GG : Nodes, Elements = 383 1254
AFLR3 GG : Nodes, Elements = 399 1302
AFLR3 GG : Nodes, Elements = 399 1374
AFLR3 GG : Nodes, Elements = 399 1350
AFLR3 GG : Nodes, Elements = 403 1362
AFLR3 GG : Nodes, Elements = 403 1377
AFLR3 GG : Nodes, Elements = 403 1376
AFLR3 : CPU Time = 0.004 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 403 1376
AFLR3 QI : Nodes, Elements = 402 1370
AFLR3 QI : Nodes, Elements = 402 1376
AFLR3 QI : Nodes, Elements = 402 1371
AFLR3 QI : Nodes, Elements = 402 1365
AFLR3 QI : Nodes, Elements = 402 1368
AFLR3 QI : Nodes, Elements = 402 1364
AFLR3 QI : Nodes, Elements = 402 1363
AFLR3 : CPU Time = 0.002 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1363
UG3 : Min, Max Ang = 21.47 133.3
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1363
UG3 : Min Vol = 1.71e-06
UG3 : Average Vol = 1.35e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1363
UG3 : Min, Max Q = 0.599 0.999
UG3 : Average Q = 0.859
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 1363
UG3 : Min, Max Ang = 21.47 133.3
UG3 : Average Angle = 70.1
UG3 : No. Angle>160.0 = 0
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 0.0184
UG3 : No. Tet Elems = 1363
UG3 : Min Vol = 1.71e-06
UG3 : Average Vol = 1.35e-05
UG3 : Total-Tet-Vol = 0.0184
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 = 1363
UG3 : Min, Max Q = 0.649 1
UG3 : Average Q = 0.878
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 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
OVERALL : CPU Time = 0.019 seconds
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 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 : EGADS TESS CREATED
EGADS : CHECK TESS GLOBAL 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
Volume mesh:
Number of nodes = 3789
Number of elements = 18890
Number of triangles = 5566
Number of quadrilatarals = 0
Number of tetrahedrals = 13324
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
Writing exodus file ....
Block: 'tableTop', blk_id 1, num_entries 7791
Block: 'leg0', blk_id 2, num_entries 1409
Block: 'leg1', blk_id 3, num_entries 1369
Block: 'leg2', blk_id 4, num_entries 1392
Block: 'leg3', blk_id 5, num_entries 1363
Sideset: 'leg0Side', set_id 1, num_entries 598
Sideset: 'leg1Side', set_id 2, num_entries 592
Sideset: 'leg2Side', set_id 3, num_entries 598
Sideset: 'leg3Side', set_id 4, num_entries 592
Sideset: 'tableTopSide', set_id 5, num_entries 3186
Nodeset: 'edge', set_id 1, num_entries 25
Nodeset: 'face1', set_id 2, num_entries 244
Nodeset: 'face2', set_id 3, num_entries 248
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
Projecting tessellation 1 (of 5) on to new body
Projecting tessellation 2 (of 5) on to new body
Projecting tessellation 3 (of 5) on to new body
Projecting tessellation 4 (of 5) on to new body
Projecting tessellation 5 (of 5) on to new body
real 0m2.928s
user 0m2.406s
sys 0m0.464s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_aflr_table_morph_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_tetgen_table_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
plato_tetgen_table_PyTest.py test;
+ python -u plato_tetgen_table_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 642
Number of elements = 1280
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1280
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 1069
Number of elements = 2134
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2134
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 1069
Number of elements = 2134
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2134
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 1069
Number of elements = 2134
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2134
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 1069
Number of elements = 2134
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2134
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4918
Total number of elements = 9816
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Body 1 number of surface: nodes - 642, elements - 1280
Body 2 number of surface: nodes - 1069, elements - 2134
Body 3 number of surface: nodes - 1069, elements - 2134
Body 4 number of surface: nodes - 1069, elements - 2134
Body 5 number of surface: nodes - 1069, elements - 2134
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.033781
Creating surface mesh ...
Surface mesh seconds: 0.002211
Recovering boundaries...
Boundary recovery seconds: 0.008343
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.000865
Recovering Delaunayness...
Delaunay recovery seconds: 0.011362
Refining mesh...
Refinement seconds: 0.001619
Improving mesh...
Mesh improvement seconds: 0.001672
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000448
Total running seconds: 0.060427
Statistics:
Input points: 642
Input facets: 1280
Input segments: 1920
Input holes: 0
Input regions: 1
Mesh points: 642
Mesh tetrahedra: 1722
Mesh faces: 4084
Mesh faces on exterior boundary: 1280
Mesh faces on input facets: 1280
Mesh edges on input segments: 1920
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.180422
Creating surface mesh ...
Surface mesh seconds: 0.004427
Recovering boundaries...
Boundary recovery seconds: 0.016597
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.00393
Recovering Delaunayness...
Delaunay recovery seconds: 0.046142
Refining mesh...
Refinement seconds: 0.145438
Smoothing vertices...
Mesh smoothing seconds: 0.192645
Improving mesh...
Mesh improvement seconds: 0.009504
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001279
Total running seconds: 0.600678
Statistics:
Input points: 1069
Input facets: 2134
Input segments: 3201
Input holes: 0
Input regions: 2
Mesh points: 1317
Mesh tetrahedra: 4475
Mesh faces: 10017
Mesh faces on exterior boundary: 2134
Mesh faces on input facets: 2134
Mesh edges on input segments: 3201
Steiner points inside domain: 248
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.170425
Creating surface mesh ...
Surface mesh seconds: 0.003772
Recovering boundaries...
Boundary recovery seconds: 0.010353
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.003265
Recovering Delaunayness...
Delaunay recovery seconds: 0.045275
Refining mesh...
Refinement seconds: 0.155952
Smoothing vertices...
Mesh smoothing seconds: 0.129382
Improving mesh...
Mesh improvement seconds: 0.005176
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000685
Total running seconds: 0.524425
Statistics:
Input points: 1069
Input facets: 2134
Input segments: 3201
Input holes: 0
Input regions: 3
Mesh points: 1308
Mesh tetrahedra: 4409
Mesh faces: 9885
Mesh faces on exterior boundary: 2134
Mesh faces on input facets: 2134
Mesh edges on input segments: 3201
Steiner points inside domain: 239
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.224568
Creating surface mesh ...
Surface mesh seconds: 0.004713
Recovering boundaries...
Boundary recovery seconds: 0.012737
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.003436
Recovering Delaunayness...
Delaunay recovery seconds: 0.048304
Refining mesh...
Refinement seconds: 0.172332
Smoothing vertices...
Mesh smoothing seconds: 0.145394
Improving mesh...
Mesh improvement seconds: 0.006854
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.001175
Total running seconds: 0.619752
Statistics:
Input points: 1069
Input facets: 2134
Input segments: 3201
Input holes: 0
Input regions: 4
Mesh points: 1316
Mesh tetrahedra: 4453
Mesh faces: 9973
Mesh faces on exterior boundary: 2134
Mesh faces on input facets: 2134
Mesh edges on input segments: 3201
Steiner points inside domain: 247
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.199379
Creating surface mesh ...
Surface mesh seconds: 0.005402
Recovering boundaries...
Boundary recovery seconds: 0.010336
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.004135
Recovering Delaunayness...
Delaunay recovery seconds: 0.056976
Refining mesh...
Refinement seconds: 0.183349
Smoothing vertices...
Mesh smoothing seconds: 0.14744
Improving mesh...
Mesh improvement seconds: 0.006421
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.000769
Total running seconds: 0.614356
Statistics:
Input points: 1069
Input facets: 2134
Input segments: 3201
Input holes: 0
Input regions: 5
Mesh points: 1321
Mesh tetrahedra: 4489
Mesh faces: 10045
Mesh faces on exterior boundary: 2134
Mesh faces on input facets: 2134
Mesh edges on input segments: 3201
Steiner points inside domain: 252
Done meshing using TetGen!
Writing VTK file: volume.vtk....
Finished writing VTK file
Writing exodus file ....
Block: 'tableTop', blk_id 1, num_entries 1722
Block: 'leg0', blk_id 2, num_entries 4475
Block: 'leg1', blk_id 3, num_entries 4409
Block: 'leg2', blk_id 4, num_entries 4453
Block: 'leg3', blk_id 5, num_entries 4489
Sideset: 'leg0Side', set_id 1, num_entries 2134
Sideset: 'leg1Side', set_id 2, num_entries 2134
Sideset: 'leg2Side', set_id 3, num_entries 2134
Sideset: 'leg3Side', set_id 4, num_entries 2134
Sideset: 'tableTopSide', set_id 5, num_entries 1280
Nodeset: 'edge', set_id 1, num_entries 17
Nodeset: 'face1', set_id 2, num_entries 99
Nodeset: 'face2', set_id 3, num_entries 99
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
real 0m5.411s
user 0m4.769s
sys 0m0.503s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_tetgen_table_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_tetgen_cyli_box_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
plato_tetgen_cyli_box_PyTest.py test;
+ python -u plato_tetgen_cyli_box_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
EGADS Warning: Loop 2 marked with -1
EGADS Warning: Loop 2 marked with -1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 3605
Number of elements = 7334
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 7334
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 3605
Total number of elements = 7334
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = box, index = 1
Name = cyl2, index = 2
Name = box;cyl2, index = 3
Name = cyl1, index = 4
Name = cyl1;box;cyl2, index = 5
Number of surface: nodes - 3605, elements - 7334
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.353959
Creating surface mesh ...
Surface mesh seconds: 0.022635
Recovering boundaries...
Boundary recovery seconds: 0.072848
Removing exterior tetrahedra ...
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.006501
Recovering Delaunayness...
Delaunay recovery seconds: 0.324869
Refining mesh...
Refinement seconds: 0.622753
Smoothing vertices...
Mesh smoothing seconds: 0.78988
Improving mesh...
Mesh improvement seconds: 0.030198
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.004388
Total running seconds: 2.22837
Statistics:
Input points: 3605
Input facets: 7334
Input segments: 10937
Input holes: 0
Input regions: 3
Mesh points: 5607
Mesh tetrahedra: 29303
Mesh faces: 60225
Mesh faces on exterior boundary: 3238
Mesh faces on input facets: 7334
Mesh edges on input segments: 10937
Steiner points inside domain: 2002
Done meshing using TetGen!
Writing VTK file: volume.vtk....
Finished writing VTK file
Writing exodus file ....
Block: 'a', blk_id 1, num_entries 5457
Block: 'b', blk_id 2, num_entries 11036
Block: 'c', blk_id 3, num_entries 12810
Sideset: 'box', set_id 1, num_entries 3238
Sideset: 'cyl1', set_id 2, num_entries 2120
Sideset: 'cyl2', set_id 3, num_entries 2310
Finished writing Exodus file
real 0m5.753s
user 0m5.319s
sys 0m0.455s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_tetgen_cyli_box_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'plato_aflr_tetgen_table_PyTest.py test;'
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
plato_aflr_tetgen_table_PyTest.py test;
+ python -u plato_aflr_tetgen_table_PyTest.py -outLevel=0
+ tee -a /Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64/ESP/DARWIN64/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.14.6
AFLR2 : Version Date 11/20/22 @ 09:21PM
AFLR2 : Compile OS Darwin 22.1.0 x86_64
AFLR2 : Compile Date 11/20/22 @ 09:24PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.3.15
AFLR4 : Version Date 12/07/22 @ 10:53AM
AFLR4 : Compile OS Darwin 22.1.0 x86_64
AFLR4 : Compile Date 12/07/22 @ 10:53AM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.23
EGADS : OpenCASCADE Version 7.4.1
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 5 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 6 Faces
EGADS : Body 0 has 12 Edges
EGADS : Body 0 has 6 Loops
EGADS : Body 0 has 8 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 4 Faces
EGADS : Body 1 has 6 Edges
EGADS : Body 1 has 4 Loops
EGADS : Body 1 has 4 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 4 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 4 Loops
EGADS : Body 2 has 4 Nodes
EGADS : Body 3 is a SolidBody
EGADS : Body 3 has 1 Shells
EGADS : Body 3 has 4 Faces
EGADS : Body 3 has 6 Edges
EGADS : Body 3 has 4 Loops
EGADS : Body 3 has 4 Nodes
EGADS : Body 4 is a SolidBody
EGADS : Body 4 has 1 Shells
EGADS : Body 4 has 4 Faces
EGADS : Body 4 has 6 Edges
EGADS : Body 4 has 4 Loops
EGADS : Body 4 has 4 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 0 1 3 4 5 6
EGADS : 2 Yes 0 0 1 0 1 3 4 5 6
EGADS : 3 Yes 0 0 1 0 1 1 2 5 6
EGADS : 4 Yes 0 0 1 0 1 1 2 5 6
EGADS : 5 Yes 0 0 1 0 1 1 2 3 4
EGADS : 6 Yes 0 0 1 0 1 1 2 3 4
EGADS : 7 Yes 1 0 1 0 1 8 9 10
EGADS : 8 Yes 1 0 1 0 1 7 9 10
EGADS : 9 Yes 1 0 1 0 1 7 8
EGADS : 10 Yes 1 0 1 0 1 7 8
EGADS : 11 Yes 2 0 1 0 1 12 13 14
EGADS : 12 Yes 2 0 1 0 1 11 13 14
EGADS : 13 Yes 2 0 1 0 1 11 12
EGADS : 14 Yes 2 0 1 0 1 11 12
EGADS : 15 Yes 3 0 1 0 1 16 17 18
EGADS : 16 Yes 3 0 1 0 1 15 17 18
EGADS : 17 Yes 3 0 1 0 1 15 16
EGADS : 18 Yes 3 0 1 0 1 15 16
EGADS : 19 Yes 4 0 1 0 1 20 21 22
EGADS : 20 Yes 4 0 1 0 1 19 21 22
EGADS : 21 Yes 4 0 1 0 1 19 20
EGADS : 22 Yes 4 0 1 0 1 19 20
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 2 -3 -4
EGADS : 2 -5 8 7 -6
EGADS : 3 9 5 -10 -1
EGADS : 4 -11 3 12 -7
EGADS : 5 4 11 -8 -9
EGADS : 6 -2 10 6 -12
EGADS : 7 -13 -14 15 16
EGADS : 8 17 14 -18 -16
EGADS : 9 13 18
EGADS : 10 -15 -17
EGADS : 11 -19 -20 21 22
EGADS : 12 23 20 -24 -22
EGADS : 13 19 24
EGADS : 14 -21 -23
EGADS : 15 -25 -26 27 28
EGADS : 16 29 26 -30 -28
EGADS : 17 25 30
EGADS : 18 -27 -29
EGADS : 19 -31 -32 33 34
EGADS : 20 35 32 -36 -34
EGADS : 21 31 36
EGADS : 22 -33 -35
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 : 17 17
EGADS : 18 18
EGADS : 19 19
EGADS : 20 20
EGADS : 21 21
EGADS : 22 22
EGADS : Loop Edges Information
EGADS : Loop Active Sense Edges
EGADS : 1 Yes 1 1 2 -3 -4
EGADS : 2 Yes 1 -5 8 7 -6
EGADS : 3 Yes 1 9 5 -10 -1
EGADS : 4 Yes 1 -11 3 12 -7
EGADS : 5 Yes 1 4 11 -8 -9
EGADS : 6 Yes 1 -2 10 6 -12
EGADS : 7 Yes 1 -13 -14 15 16
EGADS : 8 Yes 1 17 14 -18 -16
EGADS : 9 Yes 1 13 18
EGADS : 10 Yes 1 -15 -17
EGADS : 11 Yes 1 -19 -20 21 22
EGADS : 12 Yes 1 23 20 -24 -22
EGADS : 13 Yes 1 19 24
EGADS : 14 Yes 1 -21 -23
EGADS : 15 Yes 1 -25 -26 27 28
EGADS : 16 Yes 1 29 26 -30 -28
EGADS : 17 Yes 1 25 30
EGADS : 18 Yes 1 -27 -29
EGADS : 19 Yes 1 -31 -32 33 34
EGADS : 20 Yes 1 35 32 -36 -34
EGADS : 21 Yes 1 31 36
EGADS : 22 Yes 1 -33 -35
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 2 1 1 1 3
EGADS : 2 0 Yes 1 3 1 1 6
EGADS : 3 0 Yes 4 3 1 1 4
EGADS : 4 0 Yes 2 4 1 1 5
EGADS : 5 0 Yes 6 5 1 2 3
EGADS : 6 0 Yes 5 7 1 2 6
EGADS : 7 0 Yes 8 7 1 2 4
EGADS : 8 0 Yes 6 8 1 2 5
EGADS : 9 0 Yes 2 6 1 3 5
EGADS : 10 0 Yes 1 5 1 3 6
EGADS : 11 0 Yes 4 8 1 4 5
EGADS : 12 0 Yes 3 7 1 4 6
EGADS : 13 1 Yes 10 9 1 7 9
EGADS : 14 1 Yes 11 10 1 7 8
EGADS : 15 1 Yes 11 12 1 7 10
EGADS : 16 1 Yes 12 9 1 7 8
EGADS : 17 1 Yes 12 11 1 8 10
EGADS : 18 1 Yes 9 10 1 8 9
EGADS : 19 2 Yes 14 13 1 11 13
EGADS : 20 2 Yes 15 14 1 11 12
EGADS : 21 2 Yes 15 16 1 11 14
EGADS : 22 2 Yes 16 13 1 11 12
EGADS : 23 2 Yes 16 15 1 12 14
EGADS : 24 2 Yes 13 14 1 12 13
EGADS : 25 3 Yes 18 17 1 15 17
EGADS : 26 3 Yes 19 18 1 15 16
EGADS : 27 3 Yes 19 20 1 15 18
EGADS : 28 3 Yes 20 17 1 15 16
EGADS : 29 3 Yes 20 19 1 16 18
EGADS : 30 3 Yes 17 18 1 16 17
EGADS : 31 4 Yes 22 21 1 19 21
EGADS : 32 4 Yes 23 22 1 19 20
EGADS : 33 4 Yes 23 24 1 19 22
EGADS : 34 4 Yes 24 21 1 19 20
EGADS : 35 4 Yes 24 23 1 20 22
EGADS : 36 4 Yes 21 22 1 20 21
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 0 0 0.5
EGADS : 2 Yes 0 0 0
EGADS : 3 Yes 0 0.1 0.5
EGADS : 4 Yes 0 0.1 0
EGADS : 5 Yes 0.5 0 0.5
EGADS : 6 Yes 0.5 0 0
EGADS : 7 Yes 0.5 0.1 0.5
EGADS : 8 Yes 0.5 0.1 0
EGADS : 9 Yes 0 0 0
EGADS : 10 Yes 0 0 0
EGADS : 11 Yes 0 0 0
EGADS : 12 Yes 0 0 0
EGADS : 13 Yes 0 0 0.26
EGADS : 14 Yes 0 0 0.46
EGADS : 15 Yes 0 0 0.46
EGADS : 16 Yes 0 0 0.26
EGADS : 17 Yes 0.36 0 0.26
EGADS : 18 Yes 0.36 0 0.46
EGADS : 19 Yes 0.36 0 0.46
EGADS : 20 Yes 0.36 0 0.26
EGADS : 21 Yes 0.36 0 0
EGADS : 22 Yes 0.36 0 0
EGADS : 23 Yes 0.36 0 0
EGADS : 24 Yes 0.36 0 0
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 1
AFLR4 : Min Bounding Box Length = 0.7
AFLR4 : Max Ref Bounding Box Length = 1
AFLR4 : Min Ref Bounding Box Length = 0.7
AFLR4 : Reference Length = 1
AFLR4 : BL Thickness = 0
AFLR4 : Abs Min Surf Spacing = 0.0025
AFLR4 : Min Surf Spacing = 0.005
AFLR4 : Max Surf Spacing = 0.1
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 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 STD w/BL
AFLR4 : 12 CAD geometry 0 STD w/BL
AFLR4 : 13 CAD geometry 0 STD w/BL
AFLR4 : 14 CAD geometry 0 STD w/BL
AFLR4 : 15 CAD geometry 0 STD w/BL
AFLR4 : 16 CAD geometry 0 STD w/BL
AFLR4 : 17 CAD geometry 0 STD w/BL
AFLR4 : 18 CAD geometry 0 STD w/BL
AFLR4 : 19 CAD geometry 0 STD w/BL
AFLR4 : 20 CAD geometry 0 STD w/BL
AFLR4 : 21 CAD geometry 0 STD w/BL
AFLR4 : 22 CAD geometry 0 STD w/BL
AFLR4 : Case has 5 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6
AFLR4 : Component 2 includes Definitions 7 8 9 10
AFLR4 : Component 3 includes Definitions 11 12 13 14
AFLR4 : Component 4 includes Definitions 15 16 17 18
AFLR4 : Component 5 includes Definitions 19 20 21 22
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 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR4 : Define CAD surface definition 19
AFLR4 : Define CAD surface definition 20
AFLR4 : Define CAD surface definition 21
AFLR4 : Define CAD surface definition 22
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 229 400 0
AFLR4 : Nodes, Trias,Quads= 212 366 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 230 402 0
AFLR4 : Nodes, Trias,Quads= 212 366 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 49 64 0
AFLR4 : Nodes, Trias,Quads= 34 34 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2258 4330 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2270 4354 0
AFLR4 : Nodes, Trias,Quads= 2259 4332 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 515 964 0
AFLR4 : Nodes, Trias,Quads= 413 760 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 504 942 0
AFLR4 : Nodes, Trias,Quads= 402 738 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 20764 41508 2224
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Trias = 20764 41508
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 201 348 0
AFLR4 : Nodes, Trias,Quads= 193 332 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 204 354 0
AFLR4 : Nodes, Trias,Quads= 193 332 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 46 60 0
AFLR4 : Nodes, Trias,Quads= 30 28 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2246 4306 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2249 4312 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2249 4312 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Nodes, Trias,Quads= 2244 4302 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2248 4310 0
AFLR4 : Nodes, Trias,Quads= 2245 4304 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 496 926 0
AFLR4 : Nodes, Trias,Quads= 416 766 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 502 938 0
AFLR4 : Nodes, Trias,Quads= 408 750 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 20651 41282 2208
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Nodes, Trias = 21564 43108
AFLR4 : Nodes, Trias = 22448 44876
AFLR4 : Nodes, Trias = 22540 45060
AFLR4 : Surface Grid Generation
AFLR4 : Generate optimal mesh on surface definition 1
AFLR2 : Nodes, Trias,Quads= 311 517 0
AFLR4 : Nodes, Trias,Quads= 309 513 0
AFLR4 : Generate optimal mesh on surface definition 2
AFLR2 : Nodes, Trias,Quads= 313 521 0
AFLR4 : Nodes, Trias,Quads= 309 513 0
AFLR4 : Generate optimal mesh on surface definition 3
AFLR2 : Nodes, Trias,Quads= 3277 6339 0
AFLR4 : Nodes, Trias,Quads= 1431 2647 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 1864 3566 0
AFLR4 : Nodes, Trias,Quads= 1736 3310 0
AFLR4 : Generate optimal mesh on surface definition 5
AFLR2 : Nodes, Trias,Quads= 315 525 0
AFLR4 : Nodes, Trias,Quads= 307 509 0
AFLR4 : Generate optimal mesh on surface definition 6
AFLR2 : Nodes, Trias,Quads= 318 530 0
AFLR4 : Nodes, Trias,Quads= 314 522 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2271 4352 0
AFLR4 : Generate optimal mesh on surface definition 8
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2274 4358 0
AFLR4 : Generate optimal mesh on surface definition 9
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 10
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 11
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 12
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2277 4364 0
AFLR4 : Generate optimal mesh on surface definition 13
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 14
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 15
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2271 4352 0
AFLR4 : Generate optimal mesh on surface definition 16
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2276 4362 0
AFLR4 : Generate optimal mesh on surface definition 17
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
AFLR4 : Generate optimal mesh on surface definition 19
AFLR2 : Nodes, Trias,Quads= 2301 4412 0
AFLR4 : Nodes, Trias,Quads= 2272 4354 0
AFLR4 : Generate optimal mesh on surface definition 20
AFLR2 : Nodes, Trias,Quads= 2302 4414 0
AFLR4 : Nodes, Trias,Quads= 2274 4358 0
AFLR4 : Generate optimal mesh on surface definition 21
AFLR2 : Nodes, Trias,Quads= 548 1028 0
AFLR4 : Nodes, Trias,Quads= 423 778 0
AFLR4 : Generate optimal mesh on surface definition 22
AFLR2 : Nodes, Trias,Quads= 549 1030 0
AFLR4 : Nodes, Trias,Quads= 418 768 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 24536 49052 2818
OVERALL : CPU Time = 1.291 seconds
Body 1 (of 5)
Number of nodes = 4009
Number of elements = 8014
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 8014
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 5130
Number of elements = 10256
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10256
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 5134
Number of elements = 10264
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10264
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 5132
Number of elements = 10260
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10260
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 5131
Number of elements = 10258
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 10258
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 24536
Total number of elements = 49052
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = tableTopSide, index = 1
Name = leg0Side, index = 2
Name = leg1Side, index = 3
Name = leg2Side, index = 4
Name = leg3Side, index = 5
Body 1 number of surface: nodes - 4009, elements - 8014
Body 2 number of surface: nodes - 5130, elements - 10256
Body 3 number of surface: nodes - 5134, elements - 10264
Body 4 number of surface: nodes - 5132, elements - 10260
Body 5 number of surface: nodes - 5131, elements - 10258
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.063114
Creating surface mesh ...
Surface mesh seconds: 0.015081
Recovering boundaries...
Boundary recovery seconds: 0.030037
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.004472
Recovering Delaunayness...
Delaunay recovery seconds: 0.010653
Refining mesh...
Refinement seconds: 0.148874
Smoothing vertices...
Mesh smoothing seconds: 0.177738
Improving mesh...
Mesh improvement seconds: 0.018747
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.003424
Total running seconds: 0.472485
Statistics:
Input points: 4009
Input facets: 8014
Input segments: 12021
Input holes: 0
Input regions: 1
Mesh points: 4748
Mesh tetrahedra: 15739
Mesh faces: 35485
Mesh faces on exterior boundary: 8014
Mesh faces on input facets: 8014
Mesh edges on input segments: 12021
Steiner points inside domain: 739
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.21155
Creating surface mesh ...
Surface mesh seconds: 0.024689
Recovering boundaries...
Boundary recovery seconds: 0.077817
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.046641
Recovering Delaunayness...
Delaunay recovery seconds: 0.041075
Refining mesh...
Refinement seconds: 0.379251
Smoothing vertices...
Mesh smoothing seconds: 0.321006
Improving mesh...
Mesh improvement seconds: 0.024546
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006292
Total running seconds: 1.13349
Statistics:
Input points: 5130
Input facets: 10256
Input segments: 15384
Input holes: 0
Input regions: 2
Mesh points: 6609
Mesh tetrahedra: 23414
Mesh faces: 51956
Mesh faces on exterior boundary: 10256
Mesh faces on input facets: 10256
Mesh edges on input segments: 15384
Steiner points inside domain: 1479
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.172556
Creating surface mesh ...
Surface mesh seconds: 0.027448
Recovering boundaries...
Boundary recovery seconds: 0.08275
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.040844
Recovering Delaunayness...
Delaunay recovery seconds: 0.034617
Refining mesh...
Refinement seconds: 0.422424
Smoothing vertices...
Mesh smoothing seconds: 0.426225
Improving mesh...
Mesh improvement seconds: 0.040164
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.007657
Total running seconds: 1.25521
Statistics:
Input points: 5134
Input facets: 10264
Input segments: 15396
Input holes: 0
Input regions: 3
Mesh points: 6594
Mesh tetrahedra: 23251
Mesh faces: 51634
Mesh faces on exterior boundary: 10264
Mesh faces on input facets: 10264
Mesh edges on input segments: 15396
Steiner points inside domain: 1460
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.186032
Creating surface mesh ...
Surface mesh seconds: 0.022544
Recovering boundaries...
Boundary recovery seconds: 0.078075
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.036269
Recovering Delaunayness...
Delaunay recovery seconds: 0.039179
Refining mesh...
Refinement seconds: 0.465803
Smoothing vertices...
Mesh smoothing seconds: 0.433536
Improving mesh...
Mesh improvement seconds: 0.042558
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.008103
Total running seconds: 1.31283
Statistics:
Input points: 5132
Input facets: 10260
Input segments: 15390
Input holes: 0
Input regions: 4
Mesh points: 6610
Mesh tetrahedra: 23397
Mesh faces: 51924
Mesh faces on exterior boundary: 10260
Mesh faces on input facets: 10260
Mesh edges on input segments: 15390
Steiner points inside domain: 1478
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.147576
Creating surface mesh ...
Surface mesh seconds: 0.023457
Recovering boundaries...
Boundary recovery seconds: 0.088348
Removing exterior tetrahedra ...
Warning: The 1-th region point lies outside the convex hull.
Warning: The 2-th region point lies outside the convex hull.
Warning: The 3-th region point lies outside the convex hull.
Warning: The 4-th region point lies outside the convex hull.
Spreading region attributes.
Exterior tets removal seconds: 0.043055
Recovering Delaunayness...
Delaunay recovery seconds: 0.047267
Refining mesh...
Refinement seconds: 0.443117
Smoothing vertices...
Mesh smoothing seconds: 0.397123
Improving mesh...
Mesh improvement seconds: 0.036082
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006565
Total running seconds: 1.23307
Statistics:
Input points: 5131
Input facets: 10258
Input segments: 15387
Input holes: 0
Input regions: 5
Mesh points: 6601
Mesh tetrahedra: 23305
Mesh faces: 51739
Mesh faces on exterior boundary: 10258
Mesh faces on input facets: 10258
Mesh edges on input segments: 15387
Steiner points inside domain: 1470
Done meshing using TetGen!
Writing VTK file: volume.vtk....
Finished writing VTK file
Writing exodus file ....
Block: 'tableTop', blk_id 1, num_entries 15739
Block: 'leg0', blk_id 2, num_entries 23414
Block: 'leg1', blk_id 3, num_entries 23251
Block: 'leg2', blk_id 4, num_entries 23397
Block: 'leg3', blk_id 5, num_entries 23305
Sideset: 'leg0Side', set_id 1, num_entries 10256
Sideset: 'leg1Side', set_id 2, num_entries 10264
Sideset: 'leg2Side', set_id 3, num_entries 10260
Sideset: 'leg3Side', set_id 4, num_entries 10258
Sideset: 'tableTopSide', set_id 5, num_entries 8014
Nodeset: 'edge', set_id 1, num_entries 41
Nodeset: 'face1', set_id 2, num_entries 610
Nodeset: 'face2', set_id 3, num_entries 617
Nodeset: 'node', set_id 4, num_entries 1
Finished writing Exodus file
real 0m13.947s
user 0m13.113s
sys 0m0.613s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case plato_aflr_tetgen_table_PyTest.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
Nastran
Mystran
=================================================
All tests pass!
=================================================
=================================================
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_UndefinedCaps/7.4/CAPS/STRUCTURE/DARWIN64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,CAPS/STRUCTURE,DARWIN64,macys)
[Static Analysis] Using reference build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN64,buildnode=macys #174' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality Gate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_UndefinedCaps/CASREV=7.4,ESPTEST=CAPS/STRUCTURE,ESP_ARCH=DARWIN64,buildnode=macys #176'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS
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