*Heading
 dynamic test of shell to solid coupling
** Job name: xshell2solid_dyn_s8r_c3d8_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
*Node
*Element, type=C3D8
** Region: (Section-1:Picked)
*Elset, elset=_I1, internal
** Section: Section-1
*Solid Section, elset=_I1, material=Material-1
1.,
*End Instance
**
*Instance, name=Part-2-1, part=Part-2
*Node
*Element, type=S8R
** Region: (Section-2:Picked)
*Elset, elset=_I1, internal, generate
** Section: Section-2
*Shell Section, elset=_I1, material=Material-1
0.25, 3
*End Instance
*Nset, nset=_G9, internal, instance=Part-1-1
*Elset, elset=_G9, internal, instance=Part-1-1
*Nset, nset=_G10, internal, instance=Part-2-1
*Nset, nset=_G11, internal, instance=Part-2-1
*Nset, nset=_G12, internal, instance=Part-2-1
*Nset, nset=_G13, internal, instance=Part-2-1
*Nset, nset=_G14, internal, instance=Part-2-1
*Nset, nset=_G15, internal, instance=Part-2-1
*Nset, nset=_G16, internal, instance=Part-2-1
*Nset, nset=_G17, internal, instance=Part-2-1
*Nset, nset=_G18, internal, instance=Part-1-1
*Elset, elset=_G18, internal, instance=Part-1-1
*Nset, nset=_G19, internal, instance=Part-1-1
*Elset, elset=_G19, internal, instance=Part-1-1
*Nset, nset=_G20, internal, instance=Part-2-1
*Nset, nset=_G21, internal, instance=Part-1-1
*Elset, elset=_G20, internal, instance=Part-2-1
*Elset, elset=_Surf-1_S3, internal, instance=Part-1-1
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_S3, S3
*Elset, elset=_Surf-2_E4, internal, instance=Part-2-1
*Elset, elset=_Surf-2_E2, internal, instance=Part-2-1
*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
*Controls,Parameters=field
,0.0,
*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