*HEADING
1 X 4 mesh for cantilever bending problem with C3D10M elements.
**
*NODE
1, 0., 0.
2, 0.75, 0.
3, 1.5, 0.
4, 2.25, 0.
5, 3., 0.
6, 3.75, 0.
7, 4.5, 0.
8, 5.25, 0.
9, 6., 0.
10, 0., 0.1
11, 0.75, 0.1
12, 1.5, 0.1
13, 2.25, 0.1
14, 3., 0.1
15, 3.75, 0.1
16, 4.5, 0.1
17, 5.25, 0.1
18, 6., 0.1
19, 0., 0.2
20, 0.75, 0.2
21, 1.5, 0.2
22, 2.25, 0.2
23, 3., 0.2
24, 3.75, 0.2
25, 4.5, 0.2
26, 5.25, 0.2
27, 6., 0.2
*NODE,NSET=MID
28, 0., 0., 0.005
29, 0.75, 0., 0.005
30, 1.5, 0., 0.005
31, 2.25, 0., 0.005
32, 3., 0., 0.005
33, 3.75, 0., 0.005
34, 4.5, 0., 0.005
35, 5.25, 0., 0.005
36, 6., 0., 0.005
37, 0., 0.1, 0.005
38, 1.5, 0.1, 0.005
39, 3., 0.1, 0.005
40, 4.5, 0.1, 0.005
41, 6., 0.1, 0.005
42, 0., 0.2, 0.005
43, 0.75, 0.2, 0.005
44, 1.5, 0.2, 0.005
45, 2.25, 0.2, 0.005
46, 3., 0.2, 0.005
47, 3.75, 0.2, 0.005
48, 4.5, 0.2, 0.005
49, 5.25, 0.2, 0.005
50, 6., 0.2, 0.005
*NODE
51, 0., 0., 0.01
52, 0.75, 0., 0.01
53, 1.5, 0., 0.01
54, 2.25, 0., 0.01
55, 3., 0., 0.01
56, 3.75, 0., 0.01
57, 4.5, 0., 0.01
58, 5.25, 0., 0.01
59, 6., 0., 0.01
60, 0., 0.1, 0.01
61, 0.75, 0.1, 0.01
62, 1.5, 0.1, 0.01
63, 2.25, 0.1, 0.01
64, 3., 0.1, 0.01
65, 3.75, 0.1, 0.01
66, 4.5, 0.1, 0.01
67, 5.25, 0.1, 0.01
68, 6., 0.1, 0.01
69, 0., 0.2, 0.01
70, 0.75, 0.2, 0.01
71, 1.5, 0.2, 0.01
72, 2.25, 0.2, 0.01
73, 3., 0.2, 0.01
74, 3.75, 0.2, 0.01
75, 4.5, 0.2, 0.01
76, 5.25, 0.2, 0.01
77, 6., 0.2, 0.01
**
**
*ELEMENT, TYPE=C3D10M, ELSET=EALL
1, 1, 19, 51, 3, 10, 37, 28,
2, 11, 29
2, 69, 51, 19, 71, 60, 37, 42,
70, 61, 43
3, 21, 3, 71, 19, 12, 38, 44,
20, 11, 43
4, 53, 71, 3, 51, 62, 38, 30,
52, 61, 29
5, 3, 19, 51, 71, 11, 37, 29,
38, 43, 61
6, 21, 71, 3, 23, 44, 38, 12,
22, 45, 13
7, 53, 3, 71, 55, 30, 38, 62,
54, 31, 63
8, 5, 55, 23, 3, 32, 39, 14,
4, 31, 13
9, 73, 23, 55, 71, 46, 39, 64,
72, 45, 63
10, 3, 23, 71, 55, 13, 45, 38,
31, 39, 63
11, 5, 23, 55, 7, 14, 39, 32,
6, 15, 33
12, 73, 55, 23, 75, 64, 39, 46,
74, 65, 47
13, 25, 7, 75, 23, 16, 40, 48,
24, 15, 47
14, 57, 75, 7, 55, 66, 40, 34,
56, 65, 33
15, 7, 23, 55, 75, 15, 39, 33,
40, 47, 65
16, 25, 75, 7, 27, 48, 40, 16,
26, 49, 17
17, 57, 7, 75, 59, 34, 40, 66,
58, 35, 67
18, 9, 59, 27, 7, 36, 41, 18,
8, 35, 17
19, 77, 27, 59, 75, 50, 41, 68,
76, 49, 67
20, 7, 27, 75, 59, 17, 49, 40,
35, 41, 67
*SOLID SECTION,ELSET=EALL,MATERIAL=A1,controls=ctr
*section controls,name=ctr,hourglass=stiffness
*MATERIAL,NAME=A1
*ELASTIC
1.E8,0.
**
** step 1,Default
**
*STEP, PERTURBATION
*STATIC
**
** fix
**
*BOUNDARY
1, 1,, 0.
1, 2,, 0.
1, 3,, 0.
10, 1,, 0.
10, 2,, 0.
10, 3,, 0.
19, 1,, 0.
19, 2,, 0.
19, 3,, 0.
28, 1,, 0.
28, 2,, 0.
28, 3,, 0.
37, 1,, 0.
37, 2,, 0.
37, 3,, 0.
42, 1,, 0.
42, 2,, 0.
42, 3,, 0.
51, 1,, 0.
51, 2,, 0.
51, 3,, 0.
60, 1,, 0.
60, 2,, 0.
60, 3,, 0.
69, 1,, 0.
69, 2,, 0.
69, 3,, 0.
MID, 3,, 0.
**
** load
**
*CLOAD, OP=NEW
9, 2, -0.25
27, 2, -0.25
59, 2, -0.25
77, 2, -0.25
**
*NODE FILE
U,
*OUTPUT,FIELD
*NODE OUTPUT
U,
*EL PRINT
S,
E,
*END STEP