*Heading
static test of shell to solid coupling
** Job name: xshell2solid_s8r_c3d10_std Model name: Model-1
**
** PARTS
**
*Part, name=Part-1
*End Part
*Part, name=Part-2
*End Part
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
0., -3.06151588455594e-17, -2.22044604925031e-16
0., -3.06151588455594e-17, -2.22044604925031e-16, 0., -1., -2.22044604925031e-16, 90.
*Node
1, -0.5, 0.125, 0.
2, -0.5, -0.125, 0.
3, -0.5, -0.125, 2.
4, -0.5, 0.125, 2.
5, 0.5, -0.125, 0.
6, 0.5, -0.125, 2.
7, 0.5, 0.125, 2.
8, 0.5, 0.125, 0.
9, 0., -0.125, 0.
10, 0., -0.125, 2.
11, 0., 0.125, 2.
12, 0., 0.125, 0.
13, 0.1662656, -0.125, 0.8788859
14, -0.1662656, 0.125, 0.8788859
15, -0.5, 0., 1.
16, -0.3331328, 0.125, 0.439443
17, -0.3331328, 0., 1.439443
18, -0.3331328, 0.125, 1.439443
19, -0.5, 0., 2.
20, -0.5, 0.125, 1.
21, -0.5, 0., 0.
22, -0.5, -0.125, 1.
23, -0.3331328, 0., 0.439443
24, -0.1668672, -0.125, 0.439443
25, -0.1668672, -0.125, 1.439443
26, 0., 0., 0.8788859
27, -0.08313281, 0., 1.439443
28, -0.25, -0.125, 2.
29, -0.25, 0., 2.
30, 0.08313281, -0.125, 1.439443
31, -0.25, 0.125, 0.
32, -0.08313281, 0.125, 0.439443
33, -0.08313281, 0., 0.439443
34, 0., 0., 0.
35, -0.25, 0., 0.
36, 0.25, -0.125, 2.
37, 0.5, 0., 2.
38, 0.25, 0., 2.
39, 0.3331328, 0., 1.439443
40, 0.3331328, -0.125, 1.439443
41, -0.08313281, 0.125, 1.439443
42, 0., 0., 2.
43, -0.25, 0.125, 2.
44, 0.1668672, 0.125, 0.439443
45, 0.1668672, 0.125, 1.439443
46, 0.5, 0.125, 1.
47, 0.3331328, 0., 0.439443
48, 0.5, 0., 1.
49, 0.5, 0., 0.
50, 0.3331328, -0.125, 0.439443
51, 0.25, 0., 0.
52, 0.08313281, -0.125, 0.439443
53, 0.25, -0.125, 0.
54, 0.5, -0.125, 1.
55, -0.25, -0.125, 0.
56, 0.25, 0.125, 0.
57, 0.25, 0.125, 2.
*Element, type=C3D10I
1, 3, 14, 1, 4, 17, 16, 15, 19, 18, 20
2, 3, 2, 1, 14, 22, 21, 15, 17, 23, 16
3, 3, 2, 14, 13, 22, 23, 17, 25, 24, 26
4, 3, 10, 14, 4, 28, 27, 17, 19, 29, 18
5, 3, 14, 10, 13, 17, 27, 28, 25, 26, 30
6, 12, 14, 1, 9, 32, 16, 31, 34, 33, 35
7, 10, 7, 6, 13, 38, 37, 36, 30, 39, 40
8, 10, 14, 4, 11, 27, 18, 29, 42, 41, 43
9, 8, 7, 14, 13, 46, 45, 44, 47, 39, 26
10, 8, 5, 7, 13, 49, 48, 46, 47, 50, 39
11, 8, 13, 9, 5, 47, 52, 51, 49, 50, 53
12, 6, 7, 5, 13, 37, 48, 54, 40, 39, 50
13, 1, 9, 14, 2, 35, 33, 16, 21, 55, 23
14, 14, 13, 2, 9, 26, 24, 23, 33, 52, 55
15, 9, 13, 8, 14, 52, 47, 51, 33, 26, 44
16, 9, 14, 8, 12, 33, 44, 51, 34, 32, 56
17, 14, 10, 7, 11, 27, 38, 45, 41, 42, 57
18, 14, 7, 10, 13, 45, 38, 27, 26, 39, 30
** Region: (Section-1:Picked)
*Elset, elset=_I1, internal, generate
1, 18, 1
** Section: Section-1
*Solid Section, elset=_I1, material=Material-1
1.,
*End Instance
**
*Instance, name=Part-2-1, part=Part-2
0., 0., 0.
0., 0., 0., 1., 0., 0., 90.
*Node
1, 0., 0., 0.
2, 8., 0., 0.
3, 8., 0.5, 0.
4, 0., 0.5, 0.
5, 0., -0.5, 0.
6, 8., -0.5, 0.
7, 2., 0., 0.
8, 4., 0., 0.
9, 6., 0., 0.
10, 6., 0.5, 0.
11, 4., 0.5, 0.
12, 2., 0.5, 0.
13, 2., -0.5, 0.
14, 4., -0.5, 0.
15, 6., -0.5, 0.
16, 1., 0., 0.
17, 2., 0.25, 0.
18, 1., 0.5, 0.
19, 0., 0.25, 0.
20, 3., 0., 0.
21, 4., 0.25, 0.
22, 3., 0.5, 0.
23, 5., 0., 0.
24, 6., 0.25, 0.
25, 5., 0.5, 0.
26, 7., 0., 0.
27, 8., 0.25, 0.
28, 7., 0.5, 0.
29, 6., -0.25, 0.
30, 7., -0.5, 0.
31, 8., -0.25, 0.
32, 4., -0.25, 0.
33, 5., -0.5, 0.
34, 2., -0.25, 0.
35, 3., -0.5, 0.
36, 0., -0.25, 0.
37, 1., -0.5, 0.
*Element, type=S8R
1, 1, 7, 12, 4, 16, 17, 18, 19
2, 7, 8, 11, 12, 20, 21, 22, 17
3, 8, 9, 10, 11, 23, 24, 25, 21
4, 9, 2, 3, 10, 26, 27, 28, 24
5, 2, 9, 15, 6, 26, 29, 30, 31
6, 9, 8, 14, 15, 23, 32, 33, 29
7, 8, 7, 13, 14, 20, 34, 35, 32
8, 7, 1, 5, 13, 16, 36, 37, 34
** Region: (Section-2:Picked)
*Elset, elset=_I1, internal, generate
1, 8, 1
** Section: Section-2
*Shell Section, elset=_I1, material=Material-1
0.25, 3
*End Instance
*Nset, nset=_G9, internal, instance=Part-1-1
3, 4, 6, 7, 10, 11, 19, 28, 29, 36, 37, 38, 42, 43, 57
*Elset, elset=_G9, internal, instance=Part-1-1
4, 7, 8, 17
*Nset, nset=_G10, internal, instance=Part-2-1
3, 6
*Nset, nset=_G11, internal, instance=Part-2-1
2,
*Nset, nset=_G11a, internal, instance=Part-2-1
27, 31
*Nset, nset=_G12, internal, instance=Part-2-1
3, 6
*Nset, nset=_G13, internal, instance=Part-2-1
2,
*Nset, nset=_G14, internal, instance=Part-2-1
3, 6
*Nset, nset=_G15, internal, instance=Part-2-1
2,
*Nset, nset=_G16, internal, instance=Part-2-1
3, 6
*Nset, nset=_G17, internal, instance=Part-2-1
2,
*Nset, nset=_G18, internal, instance=Part-1-1
3, 4, 6, 7, 10, 11, 19, 28, 29, 36, 37, 38, 42, 43, 57
*Elset, elset=_G18, internal, instance=Part-1-1
4, 7, 8, 17
*Nset, nset=_G19, internal, instance=Part-1-1
3, 4, 6, 7, 10, 11, 19, 28, 29, 36, 37, 38, 42, 43, 57
*Elset, elset=_G19, internal, instance=Part-1-1
4, 7, 8, 17
*Nset, nset=_G20, internal, instance=Part-2-1
2, 3, 6, 27, 31
*Elset, elset=_G20, internal, instance=Part-2-1
4, 5
*Elset, elset=_Surf-1_S4, internal, instance=Part-1-1, generate
6, 16, 5
*Elset, elset=_Surf-1_S2, internal, instance=Part-1-1
13,
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_S4, S4
_Surf-1_S2, S2
*Elset, elset=_Surf-2_E4, internal, instance=Part-2-1
1,
*Elset, elset=_Surf-2_E2, internal, instance=Part-2-1
8,
*Surface, type=ELEMENT, name=Surf-2
_Surf-2_E4, E4
_Surf-2_E2, E2
** Constraint: Constraint-1
*Shell to solid coupling, constraint name=Constraint-1
Surf-2, Surf-1
*End Assembly
**
** MATERIALS
**
*Material, name=Material-1
*Density
1700.,
*Elastic
3e+07, 0.3
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, perturbation
bend - perturbation
*Static
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_G9, 1, 1
_G9, 2, 2
_G9, 3, 3
**
** LOADS
**
** Name: Load-1 Type: Concentrated force
*Cload
_G10, 2, -3.75
_G11, 2, -7.5
_G11a, 2, -15.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*El Print, freq=999999
*Node Print, freq=999999
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-2
**
*Step, name=Step-2, perturbation
pull - perturbation
*Static
**
** BOUNDARY CONDITIONS
**
** Name: BC-2 Type: Displacement/Rotation
*Boundary
_G18, 1, 1
_G18, 2, 2
_G18, 3, 3
**
** LOADS
**
** Name: Load-3 Type: Concentrated force
*Cload
_G10, 1, 3.75
_G11, 1, 7.5
_G11a, 1, 15.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-3
**
*Step, name=Step-3, nlgeom
bend - nonlinear
*Static
0.25, 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-3 Type: Displacement/Rotation
*Boundary
_G19, 1, 1
_G19, 2, 2
_G19, 3, 3
**
** LOADS
**
** Name: Load-5 Type: Concentrated force
*Cload
_G10, 2, -3.75
_G11, 2, -7.5
_G11a, 2, -15.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-2
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-2
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-4
**
*Step, name=Step-4, nlgeom
pull - nonlinear
*Static
0.25, 1., 1e-05, 1.
**
** LOADS
**
*Cload, Op = new
_G10, 1, 3.75
_G11, 1, 7.5
_G11a, 1, 15.
** Name: Load-5 Type: Concentrated force
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-2
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-2
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-5
**
*Step, name=Step-5, nlgeom
unload
*Static
1., 1., 1e-05, 1.
**
** LOADS
**
** Name: Load-7 Type: Concentrated force
*Cload, op=NEW
** Name: Load-8 Type: Concentrated force
*Cload, op=NEW
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-2
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-2
**
*Output, history, variable=PRESELECT
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-6
**
*Step, name=Step-6, nlgeom
rigid rotation
*Static
0.04, 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-3 Type: Displacement/Rotation
*Boundary, op=NEW
** Name: BC-4 Type: Displacement/Rotation
*Boundary, op=NEW
_G20, 1, 1
_G20, 2, 2
_G20, 3, 3
_G20, 6, 6, -1.5708
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=1
**
** FIELD OUTPUT: F-Output-2
**
*Output, field
*Node Output
U,
*Element Output
S,
**
** HISTORY OUTPUT: H-Output-2
**
*Output, history, variable=PRESELECT
*End Step