*Heading
static test of shell to solid coupling
** Job name: xshell2solid_s8r_c3d8_nb_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.
*Element, type=C3D8
1, 5, 6, 8, 7, 1, 2, 4, 3
2, 9, 10, 12, 11, 5, 6, 8, 7
** 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.
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, 7, 8, 11, 12
*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=_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, 7, 8, 11, 12
*Elset, elset=_G18, internal, instance=Part-1-1
1, 2
*Nset, nset=_G19, internal, instance=Part-1-1
3, 4, 7, 8, 11, 12
*Elset, elset=_G19, internal, instance=Part-1-1
1, 2
*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_S3, internal, instance=Part-1-1
1, 2
*Nset, nset=_G21, internal, instance=Part-1-1
1, 2, 9, 10
*Nset, nset=_G22, internal, instance=Part-1-1
5, 6
*Surface, type=NODE, name=Surf-1
_G21, 1.
_G22, 2.
*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, position tolerance=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,
*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,
*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,
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-4
**
*Step, name=Step-4, nlgeom
pull - nonlinear
*Static
0.25, 1., 1e-05, 1.
**
** LOADS
**
** Name: Load-5 Type: Concentrated force
*Cload, Op = new
_G10, 1, 3.75
_G11, 1, 7.5
_G11a, 1, 15.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-2
**
*Output, field
*Node Output
U,
*Element Output
S,
*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,
*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,
*End Step