*Heading
** test traction load in a cylindrical system
*Preprint, echo=NO, model=NO, history=YES, contact=NO
**
** PARTS
**
*Part, name=Part-1
*End Part
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*Node
*Element, type=C3D8
*Node
*Nset, nset=Part-1-1-RefPt_, internal
*Orientation, name=Ori-1, system=CYLINDRICAL
** Region: (Section-1:Picked), (Material Orientation:Picked)
*Elset, elset=_PickedSet2, internal, generate
** Section: Section-1
*Solid Section, elset=_PickedSet2, orientation=Ori-1, material=Material-1
1.,
*End Instance
*Nset, nset=_PickedSet5, internal, instance=Part-1-1
*Nset, nset=_PickedSet6, internal, instance=Part-1-1
*Elset, elset=__PickedSurf4_S2, internal, instance=Part-1-1, generate
*Surface, type=ELEMENT, name=_PickedSurf4, internal
__PickedSurf4_S2, S2
*Elset, elset=_Surf-1_S3, internal, instance=Part-1-1
*Elset, elset=_Surf-1_S4, internal, instance=Part-1-1
*Surface, type=ELEMENT, name=Surf-1
_Surf-1_S3, S3
_Surf-1_S4, S4
** Constraint: Constraint-1
*Coupling, constraint name=Constraint-1, ref node=_PickedSet5, surface=_PickedSurf4
*Kinematic
*End Assembly
**
** MATERIALS
**
*Material, name=Material-1
*Hyperelastic
100.,0.,0.01
**Material, name=Material-1
**Elastic
**100., 0.2
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, nlgeom=YES, unsymm=yes
*Static
0.01, 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_PickedSet6, 1, 1
_PickedSet6, 2, 2
_PickedSet6, 3, 3
_PickedSet6, 4, 4
_PickedSet6, 5, 5
_PickedSet6, 6, 6
**
** LOADS
**
** Name: Load-1   Type: Pressure
*Dsload,orientation=Assembly.Part-1-1.Ori-1,follower=yes,constant=no
Surf-1, trvec, 40,0,1,0.
**
** OUTPUT REQUESTS
** FIELD OUTPUT: F-Output-1
**
*Output, field, frequency=6
*Node output
u,
**
*End Step