*Heading
dynamic test of shell to solid coupling
** Job name: xshell2solid_dyn_s4r_c3d20_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., 0.125, 0.
6, 0., -0.125, 0.
7, 0., 0.125, 2.
8, 0., -0.125, 2.
9, 0.5, 0.125, 0.
10, 0.5, -0.125, 0.
11, 0.5, 0.125, 2.
12, 0.5, -0.125, 2.
13, 0., 0.125, 1.
14, 0., 0., 2.
15, 0., -0.125, 1.
16, 0., 0., 0.
17, -0.5, 0., 0.
18, -0.5, -0.125, 1.
19, -0.5, 0., 2.
20, -0.5, 0.125, 1.
21, -0.25, -0.125, 0.
22, -0.25, 0.125, 0.
23, -0.25, -0.125, 2.
24, -0.25, 0.125, 2.
25, 0.5, 0.125, 1.
26, 0.5, 0., 2.
27, 0.5, -0.125, 1.
28, 0.5, 0., 0.
29, 0.25, -0.125, 0.
30, 0.25, 0.125, 0.
31, 0.25, -0.125, 2.
32, 0.25, 0.125, 2.
*Element, type=C3D20
1, 5, 6, 8, 7, 1, 2, 4, 3, 16, 15, 14, 13, 17, 18, 19,
20, 22, 21, 23, 24
2, 9, 10, 12, 11, 5, 6, 8, 7, 28, 27, 26, 25, 16, 15, 14,
13, 30, 29, 31, 32
** Region: (Section-1:Picked)
*Elset, elset=_I1, internal
1, 2
** 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.
*Element, type=S4R
1, 1, 7, 12, 4
2, 7, 8, 11, 12
3, 8, 9, 10, 11
4, 9, 2, 3, 10
5, 2, 9, 15, 6
6, 9, 8, 14, 15
7, 8, 7, 13, 14
8, 7, 1, 5, 13
** 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, 7, 8, 11, 12, 14, 19, 23, 24, 26, 31, 32
*Elset, elset=_G9, internal, instance=Part-1-1
1, 2
*Nset, nset=_G10, internal, instance=Part-2-1
3, 6
*Nset, nset=_G11, internal, instance=Part-2-1
2,
*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, 7, 8, 11, 12, 14, 19, 23, 24, 26, 31, 32
*Elset, elset=_G18, internal, instance=Part-1-1
1, 2
*Nset, nset=_G19, internal, instance=Part-1-1
3, 4, 7, 8, 11, 12, 14, 19, 23, 24, 26, 31, 32
*Elset, elset=_G19, internal, instance=Part-1-1
1, 2
*Nset, nset=_G20, internal, instance=Part-2-1
2, 3, 6
*Elset, elset=_G20, internal, instance=Part-2-1
4, 5
*Nset, nset=_G21, internal, instance=Part-1-1
4, 8, 12
*Elset, elset=_Surf-1_S3, internal, instance=Part-1-1
1, 2
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_S3, S3
*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
frequency analysis
*Frequency, eigensolver = lanczos, SIM=NO
4, ,
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_G10, 1, 6
_G11, 1, 6
**
** 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, nlgeom
bend - nonlinear
*Static
0.25, 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-3 Type: Displacement/Rotation
*Boundary
_G14, 1, 6
_G15, 1, 6
**
** LOADS
**
** Name: Load-5 Type: Concentrated force
*Cload
_G21, 2, -60.
**
** 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-3
**
*Step, name=Step-3, nlgeom
dynamic analysis
*Dynamic, haftol=3e4
0.1, 20.,,2.
**
** LOADS
**
** Name: Load-5 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