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Larry Price
gmsh
Commits
b865bc38
Commit
b865bc38
authored
18 years ago
by
Christophe Geuzaine
Browse files
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benchmarks/3d/gasdis.geo
+217
-0
217 additions, 0 deletions
benchmarks/3d/gasdis.geo
benchmarks/bugs/needs_rand_1e-9.geo
+307
-0
307 additions, 0 deletions
benchmarks/bugs/needs_rand_1e-9.geo
with
524 additions
and
0 deletions
benchmarks/3d/gasdis.geo
0 → 100644
+
217
−
0
View file @
b865bc38
//gasdis.geo
//
//gas distribution ring
//parameters
mm
=
1e-3
;
lc1
=
0.25
*
mm
;
bigrad
=
100
*
mm
;
bigang
=
Pi
/
9
;
tuberad
=
4
*
mm
;
holerad
=
1
*
mm
;
seglength
=
3
*
mm
;
Point
(
1
)
=
{
0.0
,
0.0
,
0.0
,
lc1
};
Point
(
2
)
=
{
tuberad
,
0.0
,
0.0
,
lc1
};
Point
(
3
)
=
{
-
tuberad
,
0.0
,
0.0
,
lc1
};
Point
(
4
)
=
{
0
,
tuberad
,
0.0
,
lc1
};
Point
(
5
)
=
{
0
,
-
tuberad
,
0.0
,
lc1
};
Rotate
{
{
0
,
1
,
0
},{
0.0
,
0.0
,
0.0
},
Pi
/
6
}
{
Duplicata
{
Point
{
3
};
}}
Rotate
{
{
0
,
1
,
0
},{
0.0
,
0.0
,
0.0
},
-
Pi
/
6
}
{
Duplicata
{
Point
{
3
};
}}
Rotate
{
{
0
,
0
,
1
},{
0.0
,
0.0
,
0.0
},
Pi
/
6
}
{
Duplicata
{
Point
{
3
};
}}
Rotate
{
{
0
,
0
,
1
},{
0.0
,
0.0
,
0.0
},
-
Pi
/
6
}
{
Duplicata
{
Point
{
3
};
}}
Point
(
10
)
=
{
-
tuberad
*
Cos
(
Pi
/
6
),
0
,
0
,
lc1
};
Circle
(
1
)
=
{
9
,
10
,
6
};
Circle
(
2
)
=
{
6
,
10
,
8
};
Circle
(
3
)
=
{
8
,
10
,
7
};
Circle
(
4
)
=
{
7
,
10
,
9
};
Point
(
12
)
=
{
tuberad
,
0.0
,
seglength
,
lc1
};
Point
(
13
)
=
{
-
tuberad
,
0.0
,
seglength
,
lc1
};
Point
(
14
)
=
{
0
,
tuberad
,
seglength
,
lc1
};
Point
(
15
)
=
{
0
,
-
tuberad
,
seglength
,
lc1
};
Point
(
16
)
=
{
0
,
0
,
seglength
,
lc1
};
Point
(
17
)
=
{
tuberad
,
0.0
,
-
seglength
,
lc1
};
Point
(
18
)
=
{
-
tuberad
,
0.0
,
-
seglength
,
lc1
};
Point
(
19
)
=
{
0
,
tuberad
,
-
seglength
,
lc1
};
Point
(
20
)
=
{
0
,
-
tuberad
,
-
seglength
,
lc1
};
Point
(
21
)
=
{
0
,
0
,
-
seglength
,
lc1
};
Circle
(
6
)
=
{
13
,
16
,
14
};
Circle
(
7
)
=
{
14
,
16
,
12
};
Circle
(
8
)
=
{
12
,
16
,
15
};
Circle
(
9
)
=
{
15
,
16
,
13
};
Circle
(
10
)
=
{
18
,
21
,
19
};
Circle
(
11
)
=
{
19
,
21
,
17
};
Circle
(
12
)
=
{
17
,
21
,
20
};
Circle
(
13
)
=
{
20
,
21
,
18
};
Circle
(
14
)
=
{
9
,
1
,
4
};
Circle
(
15
)
=
{
4
,
1
,
2
};
Circle
(
16
)
=
{
2
,
1
,
5
};
Circle
(
17
)
=
{
5
,
1
,
8
};
Point
(
22
)
=
{
0
,
tuberad
,
-
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
23
)
=
{
0
,
-
tuberad
,
-
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
24
)
=
{
tuberad
,
0
,
-
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
25
)
=
{
0
,
0
,
-
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
26
)
=
{
0
,
tuberad
,
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
27
)
=
{
0
,
-
tuberad
,
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
28
)
=
{
tuberad
,
0
,
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
29
)
=
{
0
,
0
,
tuberad
*
Sin
(
Pi
/
6
),
lc1
};
Point
(
30
)
=
{
-
bigrad
,
tuberad
,
0
,
lc1
};
Point
(
31
)
=
{
-
bigrad
,
-
tuberad
,
0
,
lc1
};
Point
(
32
)
=
{
-
bigrad
,
0
,
0
,
lc1
};
Ellipse
(
18
)
=
{
6
,
29
,
26
,
26
};
Ellipse
(
19
)
=
{
7
,
25
,
22
,
22
};
Ellipse
(
20
)
=
{
6
,
29
,
27
,
27
};
Ellipse
(
21
)
=
{
7
,
25
,
23
,
23
};
Circle
(
22
)
=
{
26
,
29
,
28
};
Circle
(
23
)
=
{
28
,
29
,
27
};
Circle
(
24
)
=
{
22
,
25
,
24
};
Circle
(
25
)
=
{
24
,
25
,
23
};
Line
(
26
)
=
{
22
,
4
};
Line
(
27
)
=
{
4
,
26
};
Line
(
28
)
=
{
24
,
2
};
Line
(
29
)
=
{
2
,
28
};
Line
(
30
)
=
{
23
,
5
};
Line
(
31
)
=
{
5
,
27
};
Line
(
32
)
=
{
19
,
22
};
Line
(
33
)
=
{
20
,
23
};
Line
(
34
)
=
{
27
,
15
};
Line
(
35
)
=
{
28
,
12
};
Line
(
36
)
=
{
26
,
14
};
Line
(
37
)
=
{
18
,
7
};
Line
(
38
)
=
{
17
,
24
};
Line
(
39
)
=
{
6
,
13
};
Line
Loop
(
40
)
=
{
17
,
-
2
,
20
,
-
31
};
Ruled
Surface
(
41
)
=
{
40
};
Line
Loop
(
42
)
=
{
3
,
21
,
30
,
17
};
Ruled
Surface
(
43
)
=
{
42
};
Line
Loop
(
44
)
=
{
37
,
21
,
-
33
,
13
};
Ruled
Surface
(
45
)
=
{
44
};
Line
Loop
(
46
)
=
{
19
,
-
32
,
-
10
,
37
};
Ruled
Surface
(
47
)
=
{
46
};
Line
Loop
(
48
)
=
{
19
,
26
,
-
14
,
-
4
};
Ruled
Surface
(
49
)
=
{
48
};
Line
Loop
(
50
)
=
{
14
,
27
,
-
18
,
-
1
};
Ruled
Surface
(
51
)
=
{
50
};
Line
Loop
(
52
)
=
{
30
,
-
16
,
-
28
,
25
};
Ruled
Surface
(
53
)
=
{
52
};
Line
Loop
(
54
)
=
{
31
,
-
23
,
-
29
,
16
};
Ruled
Surface
(
55
)
=
{
54
};
Line
Loop
(
56
)
=
{
28
,
-
15
,
-
26
,
24
};
Ruled
Surface
(
57
)
=
{
56
};
Line
Loop
(
58
)
=
{
32
,
24
,
-
38
,
-
11
};
Ruled
Surface
(
59
)
=
{
58
};
Line
Loop
(
60
)
=
{
25
,
-
33
,
-
12
,
38
};
Ruled
Surface
(
61
)
=
{
60
};
Line
Loop
(
62
)
=
{
27
,
22
,
-
29
,
-
15
};
Ruled
Surface
(
63
)
=
{
62
};
Line
Loop
(
64
)
=
{
39
,
-
9
,
-
34
,
-
20
};
Ruled
Surface
(
65
)
=
{
64
};
Line
Loop
(
66
)
=
{
18
,
36
,
-
6
,
-
39
};
Ruled
Surface
(
67
)
=
{
66
};
Line
Loop
(
68
)
=
{
36
,
7
,
-
35
,
-
22
};
Ruled
Surface
(
69
)
=
{
68
};
Line
Loop
(
70
)
=
{
8
,
-
34
,
-
23
,
35
};
Ruled
Surface
(
71
)
=
{
70
};
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
2
*
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
3
*
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
4
*
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
5
*
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Rotate
{
{
0.0
,
1.0
,
0.0
},{
-
bigrad
,
0.0
,
0.0
},
6
*
bigang
}
{
Duplicata
{
Surface
{
41
,
43
,
45
,
47
,
49
,
51
,
53
,
55
,
57
,
59
,
61
,
63
,
65
,
67
,
69
,
71
};
}}
Circle
(
534
)
=
{
1620
,
31
,
1168
};
Circle
(
535
)
=
{
1615
,
32
,
1157
};
Circle
(
536
)
=
{
1658
,
32
,
1299
};
Circle
(
537
)
=
{
1640
,
30
,
1183
};
Circle
(
538
)
=
{
1349
,
31
,
897
};
Circle
(
539
)
=
{
1344
,
32
,
886
};
Circle
(
540
)
=
{
1369
,
30
,
912
};
Circle
(
541
)
=
{
1387
,
32
,
1028
};
Circle
(
542
)
=
{
1073
,
32
,
615
};
Circle
(
543
)
=
{
1116
,
32
,
757
};
Circle
(
544
)
=
{
1078
,
31
,
626
};
Circle
(
545
)
=
{
1098
,
30
,
641
};
Circle
(
546
)
=
{
802
,
32
,
344
};
Circle
(
547
)
=
{
807
,
31
,
355
};
Circle
(
548
)
=
{
827
,
30
,
370
};
Circle
(
549
)
=
{
845
,
32
,
486
};
Circle
(
550
)
=
{
531
,
32
,
73
};
Circle
(
551
)
=
{
215
,
32
,
574
};
Circle
(
552
)
=
{
99
,
30
,
556
};
Circle
(
553
)
=
{
536
,
31
,
84
};
Circle
(
554
)
=
{
260
,
32
,
18
};
Circle
(
555
)
=
{
17
,
32
,
303
};
Circle
(
556
)
=
{
20
,
31
,
265
};
Circle
(
557
)
=
{
285
,
30
,
19
};
Line
Loop
(
558
)
=
{
534
,
433
,
-
536
,
533
};
Ruled
Surface
(
559
)
=
{
558
};
Line
Loop
(
560
)
=
{
536
,
429
,
-
537
,
529
};
Ruled
Surface
(
561
)
=
{
560
};
Line
Loop
(
562
)
=
{
534
,
394
,
-
535
,
519
};
Ruled
Surface
(
563
)
=
{
562
};
Line
Loop
(
564
)
=
{
535
,
-
398
,
-
537
,
525
};
Ruled
Surface
(
565
)
=
{
564
};
Line
Loop
(
566
)
=
{
442
,
538
,
317
,
-
539
};
Ruled
Surface
(
567
)
=
{
566
};
Line
Loop
(
568
)
=
{
539
,
-
321
,
-
540
,
448
};
Ruled
Surface
(
569
)
=
{
568
};
Line
Loop
(
570
)
=
{
540
,
-
352
,
-
541
,
-
452
};
Ruled
Surface
(
571
)
=
{
570
};
Line
Loop
(
572
)
=
{
541
,
-
356
,
-
538
,
-
456
};
Ruled
Surface
(
573
)
=
{
572
};
Line
Loop
(
574
)
=
{
542
,
-
244
,
-
545
,
371
};
Ruled
Surface
(
575
)
=
{
574
};
Line
Loop
(
576
)
=
{
545
,
-
275
,
-
543
,
-
375
};
Ruled
Surface
(
577
)
=
{
576
};
Line
Loop
(
578
)
=
{
542
,
-
240
,
-
544
,
-
365
};
Ruled
Surface
(
579
)
=
{
578
};
Line
Loop
(
580
)
=
{
544
,
279
,
-
543
,
379
};
Ruled
Surface
(
581
)
=
{
580
};
Ruled
Surface
(
582
)
=
{
576
};
Line
Loop
(
583
)
=
{
546
,
-
163
,
-
547
,
-
288
};
Ruled
Surface
(
584
)
=
{
583
};
Line
Loop
(
585
)
=
{
202
,
-
549
,
302
,
547
};
Ruled
Surface
(
586
)
=
{
585
};
Line
Loop
(
587
)
=
{
549
,
198
,
-
548
,
298
};
Ruled
Surface
(
588
)
=
{
587
};
Line
Loop
(
589
)
=
{
167
,
-
546
,
-
294
,
548
};
Ruled
Surface
(
590
)
=
{
589
};
Line
Loop
(
591
)
=
{
217
,
550
,
-
90
,
552
};
Ruled
Surface
(
592
)
=
{
591
};
Line
Loop
(
593
)
=
{
550
,
-
86
,
-
553
,
-
211
};
Ruled
Surface
(
594
)
=
{
593
};
Line
Loop
(
595
)
=
{
225
,
553
,
125
,
551
};
Ruled
Surface
(
596
)
=
{
595
};
Line
Loop
(
597
)
=
{
221
,
-
551
,
121
,
552
};
Ruled
Surface
(
598
)
=
{
597
};
Line
Loop
(
599
)
=
{
554
,
-
13
,
556
,
-
134
};
Ruled
Surface
(
600
)
=
{
599
};
Line
Loop
(
601
)
=
{
556
,
-
148
,
-
555
,
12
};
Ruled
Surface
(
602
)
=
{
601
};
Line
Loop
(
603
)
=
{
10
,
-
557
,
140
,
554
};
Ruled
Surface
(
604
)
=
{
603
};
Line
Loop
(
605
)
=
{
557
,
11
,
555
,
-
144
};
Ruled
Surface
(
606
)
=
{
605
};
Line
Loop
(
607
)
=
{
7
,
8
,
9
,
6
};
Plane
Surface
(
608
)
=
{
607
};
Physical
Surface
(
609
)
=
{
67
,
608
,
69
,
63
,
608
,
51
,
65
,
71
,
55
,
41
,
49
,
57
,
59
,
53
,
43
,
47
,
604
,
45
,
61
,
606
,
602
,
600
,
137
,
142
,
127
,
97
,
132
,
147
,
112
,
92
,
92
,
72
,
107
,
117
,
87
,
77
,
102
,
598
,
122
,
82
,
592
,
594
,
596
,
214
,
219
,
224
,
209
,
174
,
204
,
184
,
149
,
154
,
179
,
189
,
169
,
159
,
199
,
586
,
194
,
164
,
590
,
584
,
588
,
286
,
301
,
296
,
291
,
226
,
261
,
281
,
251
,
256
,
231
,
246
,
266
,
276
,
236
,
241
,
271
,
582
,
582
,
582
,
581
,
575
,
579
,
582
,
378
,
363
,
368
,
373
,
338
,
303
,
328
,
358
,
333
,
343
,
323
,
308
,
313
,
318
,
348
,
353
,
573
,
571
,
567
,
569
,
450
,
567
,
445
,
440
,
455
,
435
,
405
,
415
,
380
,
420
,
400
,
410
,
385
,
425
,
395
,
390
,
430
,
561
,
559
,
563
,
565
,
522
,
517
,
527
,
532
,
512
,
457
,
482
,
492
,
497
,
462
,
477
,
487
,
502
,
472
,
467
,
507
};
Line
Loop
(
610
)
=
{
4
,
1
,
2
,
3
};
Plane
Surface
(
611
)
=
{
610
};
Line
Loop
(
612
)
=
{
101
,
96
,
-
78
,
74
};
Plane
Surface
(
613
)
=
{
612
};
Line
Loop
(
614
)
=
{
178
,
173
,
-
155
,
151
};
Plane
Surface
(
615
)
=
{
614
};
Line
Loop
(
616
)
=
{
255
,
250
,
-
232
,
228
};
Plane
Surface
(
617
)
=
{
616
};
Line
Loop
(
618
)
=
{
327
,
-
309
,
305
,
332
};
Plane
Surface
(
619
)
=
{
618
};
Line
Loop
(
620
)
=
{
404
,
-
386
,
382
,
409
};
Plane
Surface
(
621
)
=
{
620
};
Line
Loop
(
622
)
=
{
481
,
-
463
,
459
,
486
};
Plane
Surface
(
623
)
=
{
622
};
Line
Loop
(
624
)
=
{
506
,
475
,
-
471
,
510
};
Plane
Surface
(
625
)
=
{
624
};
Physical
Surface
(
626
)
=
{
611
,
613
,
615
,
617
,
619
,
621
,
623
};
Physical
Surface
(
627
)
=
{
625
};
Surface
Loop
(
628
)
=
{
571
,
569
,
567
,
-
440
,
-
445
,
-
405
,
-
400
,
395
,
425
,
-
420
,
-
410
,
385
,
621
,
-
380
,
-
415
,
455
,
573
,
353
,
-
333
,
308
,
619
,
-
323
,
318
,
348
,
-
343
,
358
,
-
328
,
-
368
,
373
,
582
,
575
,
-
579
,
-
236
,
241
,
-
246
,
-
266
,
-
256
,
231
,
617
,
-
251
,
281
,
296
,
-
291
,
-
590
,
164
,
-
169
,
-
189
,
-
179
,
154
,
615
,
-
174
,
204
,
219
,
-
214
,
592
,
-
594
,
-
82
,
87
,
-
92
,
-
112
,
-
102
,
77
,
613
,
-
97
,
127
,
142
,
-
137
,
604
,
47
,
-
49
,
-
57
,
-
53
,
43
,
-
611
,
-
51
,
63
,
69
,
-
67
,
-
608
,
71
,
-
65
,
-
41
,
-
55
,
-
45
,
61
,
602
,
-
600
,
-
132
,
147
,
-
107
,
-
72
,
606
,
59
,
122
,
-
596
,
224
,
-
209
,
-
149
,
-
184
,
-
598
,
117
,
-
159
,
199
,
-
586
,
-
588
,
194
,
301
,
-
286
,
-
584
,
-
226
,
-
261
,
276
,
-
581
,
378
,
-
363
,
-
303
,
-
338
,
271
,
-
313
,
450
,
435
,
-
390
,
430
,
-
559
,
563
,
565
,
-
561
,
527
,
-
522
,
-
482
,
-
477
,
472
,
502
,
-
497
,
-
487
,
462
,
623
,
-
457
,
-
517
,
532
,
-
492
,
512
,
-
467
,
507
,
-
625
};
Volume
(
629
)
=
{
628
};
This diff is collapsed.
Click to expand it.
benchmarks/bugs/needs_rand_1e-9.geo
0 → 100644
+
307
−
0
View file @
b865bc38
//Mesh.Algorithm = 1;
//Mesh.CharacteristicLengthFactor = 1;
Geometry
.
AutoCoherence
=
1
;
u
=
1e-3
;
FEM
=
0
;
/* 0->Hybrid model, 1->FEM model */
a
=
u
*
1000
;
b
=
u
*
1
;
c
=
u
*
400
;
d
=
u
*
150
;
R
=
u
*
30
;
// radius conductors
ym
=
u
*
-
250
;
// vertical offset of circular ring
M
=
u
*
1000
*
Sqrt
(
0.5
);
// circular ring inner boundary
m
=
u
*
1500
*
Sqrt
(
0.5
);
// circular ring outerr boundary
eh1
=
u
*
0.5
;
ev1
=
u
*
0.5
*
2
;
eh2
=
u
*
1.5
;
ev2
=
u
*
1.5
*
2
;
eh3
=
u
*
4.5
;
ev3
=
u
*
4.5
*
2
;
p
=
u
*
2
;
pe1
=
u
*
2
;
pe2
=
u
*
5
;
pe3
=
u
*
10
;
p
=
u
*
2
;
pe1
=
u
*
2
;
pe2
=
u
*
5
;
pe3
=
u
*
10
;
pu
=
u
*
6
*
3.6
;
pM1
=
4
*
pu
;
//4 /* For refining FEM mesh */
pM2
=
4
*
pu
;
pc
=
pu
/
3
;
b1
=
0
;
b2
=-
b
/
4
;
b3
=-
b
/
2
;
b4
=-
3
*
b
/
4
;
b5
=-
b
;
Point
(
1
)
=
{
-
a
/
2
,
b1
+
ym
,
0
,
p
};
Point
(
2
)
=
{
-
a
/
2
,
b2
+
ym
,
0
,
p
};
Point
(
3
)
=
{
a
/
2
,
b1
+
ym
,
0
,
p
};
Point
(
4
)
=
{
a
/
2
,
b2
+
ym
,
0
,
p
};
Point
(
5
)
=
{
-
a
/
2
,
b3
+
ym
,
0
,
p
};
Point
(
6
)
=
{
a
/
2
,
b3
+
ym
,
0
,
p
};
Point
(
7
)
=
{
-
a
/
2
,
b4
+
ym
,
0
,
p
};
Point
(
8
)
=
{
a
/
2
,
b4
+
ym
,
0
,
p
};
Point
(
9
)
=
{
-
a
/
2
,
b5
+
ym
,
0
,
p
};
Point
(
10
)
=
{
a
/
2
,
b5
+
ym
,
0
,
p
};
Line
(
701
)
=
{
2
,
4
};
Line
(
703
)
=
{
4
,
3
};
Line
(
704
)
=
{
3
,
1
};
Line
(
705
)
=
{
1
,
2
};
Line
(
901
)
=
{
2
,
5
};
Line
(
902
)
=
{
5
,
6
};
Line
(
903
)
=
{
6
,
4
};
Line
(
913
)
=
{
5
,
7
};
Line
(
914
)
=
{
7
,
8
};
Line
(
915
)
=
{
6
,
8
};
Line
(
916
)
=
{
8
,
10
};
Line
(
917
)
=
{
10
,
9
};
Line
(
918
)
=
{
9
,
7
};
Line
Loop
(
714
)
=
{
705
,
701
,
703
,
704
};
Plane
Surface
(
715
)
=
{
714
};
Line
Loop
(
904
)
=
{
-
903
,
-
902
,
-
901
,
701
};
Plane
Surface
(
905
)
=
{
904
};
Line
Loop
(
919
)
=
{
914
,
-
915
,
-
902
,
913
};
Plane
Surface
(
920
)
=
{
919
};
Line
Loop
(
921
)
=
{
914
,
916
,
917
,
918
};
Plane
Surface
(
922
)
=
{
921
};
Fpc
=
100
;
If
(
FEM
)
Fpc
=
1
;
EndIf
Point
(
11
)
=
{
-
c
/
2
+
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
12
)
=
{
-
c
/
2
+
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
13
)
=
{
-
c
/
2
-
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
14
)
=
{
-
c
/
2
-
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
21
)
=
{
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
22
)
=
{
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
23
)
=
{
-
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
24
)
=
{
-
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
31
)
=
{
c
/
2
+
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
32
)
=
{
c
/
2
+
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
33
)
=
{
c
/
2
-
R
/
2
,
-
b
-
d
+
ym
+
R
/
2
,
0
,
pc
*
Fpc
};
Point
(
34
)
=
{
c
/
2
-
R
/
2
,
-
b
-
d
+
ym
-
R
/
2
,
0
,
pc
*
Fpc
};
Line
(
1
)
=
{
12
,
11
};
Line
(
2
)
=
{
11
,
13
};
Line
(
3
)
=
{
13
,
14
};
Line
(
4
)
=
{
14
,
12
};
Line
(
5
)
=
{
22
,
21
};
Line
(
6
)
=
{
21
,
23
};
Line
(
7
)
=
{
23
,
24
};
Line
(
8
)
=
{
24
,
22
};
Line
(
9
)
=
{
32
,
31
};
Line
(
10
)
=
{
31
,
33
};
Line
(
11
)
=
{
33
,
34
};
Line
(
12
)
=
{
34
,
32
};
Line
Loop
(
906
)
=
{
1
,
2
,
3
,
4
};
Plane
Surface
(
907
)
=
{
906
};
Line
Loop
(
908
)
=
{
5
,
6
,
7
,
8
};
Plane
Surface
(
909
)
=
{
908
};
Line
Loop
(
910
)
=
{
9
,
10
,
11
,
12
};
Plane
Surface
(
911
)
=
{
910
};
Point
(
501
)
=
{
-
a
/
2
-
eh1
,
b1
+
ym
+
ev1
,
0
,
pe1
};
Point
(
502
)
=
{
-
a
/
2
-
eh1
,
b5
+
ym
-
ev1
,
0
,
pe1
};
Point
(
503
)
=
{
0
,
b1
+
ym
+
ev1
,
0
,
pe1
};
Point
(
504
)
=
{
0
,
b5
+
ym
-
ev1
,
0
,
pe1
};
Point
(
505
)
=
{
a
/
2
+
eh1
,
b1
+
ym
+
ev1
,
0
,
pe1
};
Point
(
506
)
=
{
a
/
2
+
eh1
,
b5
+
ym
-
ev1
,
0
,
pe1
};
Point
(
507
)
=
{
-
a
/
2
-
eh1
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe1
/
1
};
Point
(
508
)
=
{
a
/
2
+
eh1
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe1
/
1
};
Line
(
100003
)
=
{
502
,
507
};
Line
(
100004
)
=
{
501
,
503
};
Line
(
100005
)
=
{
503
,
505
};
Line
(
100006
)
=
{
505
,
508
};
Line
(
100007
)
=
{
506
,
504
};
Line
(
100008
)
=
{
504
,
502
};
Line
(
100009
)
=
{
507
,
501
};
Line
(
100010
)
=
{
508
,
506
};
Point
(
601
)
=
{
-
a
/
2
-
eh2
,
b1
+
ym
+
ev2
,
0
,
pe2
};
Point
(
602
)
=
{
-
a
/
2
-
eh2
,
b5
+
ym
-
ev2
,
0
,
pe2
};
Point
(
603
)
=
{
0
,
b1
+
ym
+
ev2
,
0
,
pe2
};
Point
(
604
)
=
{
0
,
b5
+
ym
-
ev2
,
0
,
pe2
};
Point
(
605
)
=
{
a
/
2
+
eh2
,
b1
+
ym
+
ev2
,
0
,
pe2
};
Point
(
606
)
=
{
a
/
2
+
eh2
,
b5
+
ym
-
ev2
,
0
,
pe2
};
Point
(
607
)
=
{
-
a
/
2
-
eh2
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe2
/
1
};
Point
(
608
)
=
{
a
/
2
+
eh2
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe2
/
1
};
Line
(
200003
)
=
{
602
,
607
};
Line
(
200004
)
=
{
601
,
603
};
Line
(
200005
)
=
{
603
,
605
};
Line
(
200006
)
=
{
605
,
608
};
Line
(
200007
)
=
{
606
,
604
};
Line
(
200008
)
=
{
604
,
602
};
Line
(
200009
)
=
{
607
,
601
};
Line
(
200010
)
=
{
608
,
606
};
Point
(
701
)
=
{
-
a
/
2
-
eh3
,
b1
+
ym
+
ev3
,
0
,
pe3
};
Point
(
702
)
=
{
-
a
/
2
-
eh3
,
b5
+
ym
-
ev3
,
0
,
pe3
};
Point
(
703
)
=
{
0
,
b1
+
ym
+
ev3
,
0
,
pe3
};
Point
(
704
)
=
{
0
,
b5
+
ym
-
ev3
,
0
,
pe3
};
Point
(
705
)
=
{
a
/
2
+
eh3
,
b1
+
ym
+
ev3
,
0
,
pe3
};
Point
(
706
)
=
{
a
/
2
+
eh3
,
b5
+
ym
-
ev3
,
0
,
pe3
};
Point
(
707
)
=
{
-
a
/
2
-
eh3
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe3
/
1
};
Point
(
708
)
=
{
a
/
2
+
eh3
,
ym
+
(
b1
+
b5
)
/
2
,
0
,
pe3
/
1
};
Line
(
300003
)
=
{
702
,
707
};
Line
(
300004
)
=
{
701
,
703
};
Line
(
300005
)
=
{
703
,
705
};
Line
(
300006
)
=
{
705
,
708
};
Line
(
300007
)
=
{
706
,
704
};
Line
(
300008
)
=
{
704
,
702
};
Line
(
300009
)
=
{
707
,
701
};
Line
(
300010
)
=
{
708
,
706
};
Line
Loop
(
100009
)
=
{
100004
,
100005
,
100006
,
100007
,
100008
,
100003
,
100009
,
100010
};
Line
Loop
(
100010
)
=
{
703
,
704
,
705
,
901
,
913
,
-
918
,
-
917
,
-
916
,
-
915
,
903
};
Plane
Surface
(
100011
)
=
{
100009
,
100010
};
Line
Loop
(
200009
)
=
{
200004
,
200005
,
200006
,
200007
,
200008
,
200003
,
200009
,
200010
};
Line
Loop
(
300009
)
=
{
300004
,
300005
,
300006
,
300007
,
300008
,
300003
,
300009
,
300010
};
Plane
Surface
(
200011
)
=
{
200009
,
100009
};
Plane
Surface
(
300011
)
=
{
300009
,
200009
};
AirLayer1
=
1000
;
Physical
Surface
(
AirLayer1
)
=
{
100011
};
// AirLayer1
SkinAirLayer1
=
1500
;
Physical
Line
(
SkinAirLayer1
)
=
{
100004
,
100003
,
100008
,
100007
,
100006
,
100005
,
100009
,
100010
};
// SkinAirLayer1
AirLayer2
=
2000
;
Physical
Surface
(
AirLayer2
)
=
{
200011
};
// AirLayer2
SkinAirLayer2
=
2500
;
Physical
Line
(
SkinAirLayer2
)
=
{
200004
,
200003
,
200008
,
200007
,
200006
,
200005
,
200009
,
200010
};
// SkinAirLayer2
AirLayer3
=
3000
;
Physical
Surface
(
AirLayer3
)
=
{
300011
};
// AirLayer3
SkinAirLayer3
=
3500
;
Physical
Line
(
SkinAirLayer3
)
=
{
300004
,
300003
,
300008
,
300007
,
300006
,
300005
,
300009
,
300010
};
// SkinAirLayer3
ym2
=
u
*
0
;
If
(
FEM
)
Point
(
0
)
=
{
0
,
-
ym2
,
0
,
p
};
Point
(
100
)
=
{
M
,
M
-
ym2
,
0
,
pM1
};
Point
(
101
)
=
{
-
M
,
-
M
-
ym2
,
0
,
pM1
};
Point
(
102
)
=
{
-
M
,
M
-
ym2
,
0
,
pM1
};
Point
(
103
)
=
{
M
,
-
M
-
ym2
,
0
,
pM1
};
Point
(
200
)
=
{
m
,
m
-
ym2
,
0
,
pM2
};
Point
(
201
)
=
{
-
m
,
-
m
-
ym2
,
0
,
pM2
};
Point
(
202
)
=
{
-
m
,
m
-
ym2
,
0
,
pM2
};
Point
(
203
)
=
{
m
,
-
m
-
ym2
,
0
,
pM2
};
Circle
(
25
)
=
{
103
,
0
,
100
};
Circle
(
26
)
=
{
100
,
0
,
102
};
Circle
(
27
)
=
{
102
,
0
,
101
};
Circle
(
28
)
=
{
101
,
0
,
103
};
Circle
(
35
)
=
{
203
,
0
,
200
};
Circle
(
36
)
=
{
200
,
0
,
202
};
Circle
(
37
)
=
{
202
,
0
,
201
};
Circle
(
38
)
=
{
201
,
0
,
203
};
Line
Loop
(
307
)
=
{
37
,
38
,
35
,
36
};
Line
Loop
(
720
)
=
{
27
,
28
,
25
,
26
};
Line
Loop
(
923
)
=
{
913
,
-
918
,
-
917
,
-
916
,
-
915
,
903
,
703
,
704
,
705
,
901
};
EndIf
Physical
Surface
(
100
)
=
{
907
};
// left conductor
Physical
Surface
(
150
)
=
{
909
};
// middle conductor
Physical
Surface
(
200
)
=
{
911
};
// right conductor
//Recombine Surface {715,905,920,922};
Plate
=
300
;
Physical
Surface
(
Plate
)
=
{
715
,
905
,
920
,
922
};
// plate
Physical
Line
(
700
)
=
{
-
1
,
-
2
,
-
3
,
-
4
};
// SkinLeft
Physical
Line
(
750
)
=
{
-
5
,
-
6
,
-
7
,
-
8
};
// SkinMid
Physical
Line
(
800
)
=
{
-
9
,
-
10
,
-
11
,
-
12
};
// SkinRight
SkinPlate
=
900
;
Physical
Line
(
SkinPlate
)
=
{
-
704
,
-
705
,
-
901
,
918
,
917
,
916
,
915
,
-
903
,
-
703
,
-
913
};
// SkinPlate
If
(
FEM
)
Plane
Surface
(
722
)
=
{
307
,
720
};
Plane
Surface
(
924
)
=
{
720
,
300009
,
906
,
908
,
910
};
// air
Physical
Surface
(
400
)
=
{
924
};
// air
RingIn
=
500
;
RingOut
=
600
;
Physical
Surface
(
RingIn
)
=
{
722
};
// ring
Physical
Line
(
RingOut
)
=
{
35
,
36
,
37
,
38
};
// outer boundary
EndIf
//Post Processing
xt1
=
0.8
;
xt2
=
0.6
;
yt1
=
ym
+
0.5
;
yt2
=
ym
+
1.0
;
Point
(
10001
)
=
{
xt1
,
yt1
,
0
,
p
};
Point
(
10002
)
=
{
-
xt1
,
yt1
,
0
,
p
};
Point
(
10003
)
=
{
xt2
,
yt2
,
0
,
p
};
Point
(
10004
)
=
{
-
xt2
,
yt2
,
0
,
p
};
Line
(
100001
)
=
{
10001
,
10002
};
Line
(
100002
)
=
{
10003
,
10004
};
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