*Heading
** traction loading for axisymmetric rigid and shell elements
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** 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=SAX1
** Region: (Section-1:Picked)
*Elset, elset=_PickedSet2, internal, generate
** Section: Section-1
*Shell Section, elset=_PickedSet2, material=Material-1
0.1, 5
*End Instance
**
*Instance, name=Part-2-1, part=Part-2
*Node
*Element, type=RAX2
*Node
*Nset, nset=Part-2-1-RefPt_, internal
*Elset, elset=Part-2-1, generate
*End Instance
*Nset, nset=_PickedSet19, internal, instance=Part-1-1
*Nset, nset=_PickedSet20, internal, instance=Part-2-1
*Elset, elset=_Surf-1_SNEG, internal, instance=Part-1-1, generate
*Elset, elset=_Surf-1_SPOS, internal, instance=Part-2-1, generate
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_SNEG, SNEG
*Surface, type=ELEMENT, name=Surf-2
_Surf-1_SPOS, SPOS
*Rigid Body, ref node=Part-2-1.Part-2-1-RefPt_, elset=Part-2-1.Part-2-1
*End Assembly
*Amplitude, name=Amp-1
0., 0., 1., 1.
**
** MATERIALS
**
*Material, name=Material-1
*Density
 0.0001,
*Elastic
1000., 0.3
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1
*Dynamic, Explicit
, 1.
*Bulk Viscosity
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_PickedSet19, 2, 2
_PickedSet19, 6, 6
** Name: BC-2 Type: Displacement/Rotation
*Boundary
_PickedSet20, 1, 1
_PickedSet20, 2, 2
_PickedSet20, 6, 6
**
** LOADS
**
** Name: Load-1   Type: Surface traction
*Dsload, amplitude=Amp-1
Surf-1, TRSHR, 1., 0.707107, 0.707107, 0.
Surf-2, TRSHR, 1., 0.707107, 0.707107, 0.
**
** OUTPUT REQUESTS
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, number=6
*Node output
u,rf
*End Step