*Heading
 Axisymmetic Bushing
 DSA analysis
** ----------------------------------------------------------------
** PART INSTANCE: BUSHING-1
**
*PARAMETER
R=0.0
T=0.0
*DESIGN PARAMETER
R,T
*Node,INPUT=bushing_node.inp
*Element, type=CAX4,INPUT=bushing_steel.inp
*Element, type=CAX4H,INPUT=bushing_rubber.inp
*****	Elset for Solid Section Definition
*Elset, elset=ASSEMBLY_BUSHING-1__I1
*Elset, elset=ASSEMBLY_BUSHING-1__I2
**SOLID SECTION DEFINITION
*solidsection, elset=ASSEMBLY_BUSHING-1__I1, material=STEEL-MATERIAL
 *solidsection, elset=ASSEMBLY_BUSHING-1__I2, material=RUBBER-MATERIAL
** ----------------------RIGID BODY DEFINITION
*Element, type=RAX2,INPUT=bushing_rigid.inp
*Nset, nset=ASSEMBLY_RIGID-1_RIGID-1-REFPT_
*Elset, elset=ASSEMBLY_RIGID-1_RIGID-1
*rigidbody, refnode=ASSEMBLY_RIGID-1_RIGID-1-REFPT_, elset=ASSEMBLY_RIGID-1_RIGID-1
**
** Assembly Nsets
**
*Nset, nset=ASSEMBLY_NALL
*Nset, nset=ASSEMBLY_RREF_POINT
*Elset, elset=ASSEMBLY_EALL
*Nset, nset=ASSEMBLY_OUT_ST
*Elset, elset=ASSEMBLY_OUT_ST
***********************************MATERIAL DEFINITION****************
*material, name=RUBBER-MATERIAL
*hyperelastic, n=2
11.5796, 3.47492, 0.226938, -0.177868, 0.0085253, 0., 0.
*material, name=STEEL-MATERIAL
*elastic
3E+07, 0.3
**************************************PARAMETER=R
*PARAMETER SHAPE VARIATION, PARAMETER=R
********************************************PARAMETER=T
*PARAMETER SHAPE VARIATION, PARAMETER=T
*DSA CONTROLS, FORMULATION=TOTAL
*Step, nlgeom,DSA
Point Load applied at RIGID BODY ref. point
*static, direct
1., 1.,
*boundary
ASSEMBLY_OUT_ST, 1, 1
ASSEMBLY_OUT_ST, 2, 2
*boundary
ASSEMBLY_RREF_POINT, 1, 1
ASSEMBLY_RREF_POINT, 6, 6
*cload
ASSEMBLY_RREF_POINT, 2, 2400.
*OUTPUT, FIELD
*ELEMENT OUTPUT,ELSET=ASSEMBLY_EALL
S,
*NODE OUTPUT,NSET=ASSEMBLY_NALL
U,RF
*DESIGN RESPONSE
*ELEMENT RESPONSE,ELSET=ASSEMBLY_EALL
S,
*NODE RESPONSE,NSET=ASSEMBLY_NALL
U,RF
*endstep