*Heading
** Job name: TEMP Model name: Model-1
**
** PARTS
**
*Part, name=PART-1
*End Part
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=PART-1-1, part=PART-1
*Node
*Element, type=CAX4
*Elset, elset=AXSOL
** Region: (Section-1-AXSOL:AXSOL)
*Elset, elset=_I1, internal
** Section: Section-1-AXSOL
*Solid Section, elset=_I1, material=ELMAT
1.,
*ORIENTATION,NAME=REBAR1,DEFINITION=OFFSET TO NODES
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-1
*SURFACE SECTION,ELSET=SFMAX1-1
*REBAR LAYER,ANGULAR SPACING
RB1LAYR1,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-2
*SURFACE SECTION,ELSET=SFMAX1-2
*REBAR LAYER,ANGULAR SPACING
RB1LAYR2,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMAX1,ELSET=SFMAX1-3
*SURFACE SECTION,ELSET=SFMAX1-3
*REBAR LAYER,ANGULAR SPACING
RB1LAYR3,0.040000,44.568275,0.000000,RBMAT1,0.000000,1
*EMBEDDED ELEMENT
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR1,SINGLE
AXSOL,.4,.25,.25
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR1_2,SINGLE
AXSOL,.4,.50,.25
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR1_3,SINGLE
AXSOL,.4,.75,.25
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR2,SINGLE
AXSOL,.4,.25,.5
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR2_2,SINGLE
AXSOL,.4,.50,.5
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR2_3,SINGLE
AXSOL,.4,.75,.5
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR3,SINGLE
AXSOL,.4,.25,.75
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR3_2,SINGLE
AXSOL,.4,.50,.75
*REBAR,ELEMENT=CONTINUUM,MATERIAL=RBMAT2,NAME=RB2LAYR3_3,SINGLE
AXSOL,.4,.75,.75
*End Instance
*Nset, nset=BOT, instance=PART-1-1
*Nset, nset=LEFT, instance=PART-1-1
*Nset, nset=TOP, instance=PART-1-1
*Nset, nset=EqnSet-1, instance=PART-1-1
*Nset, nset=EqnSet-2, instance=PART-1-1
*Elset, elset=__M8_S2, internal, instance=PART-1-1
*Surface, type=ELEMENT, name=_M8, internal
__M8_S2, S2
*Elset, elset=__M9_S2, internal, instance=PART-1-1
*Surface, type=ELEMENT, name=_M9, internal
__M9_S2, S2
*Equation
EqnSet-1, 1, 1.
EqnSet-2, 1, -1.
*End Assembly
**
** MATERIALS
**
*Material, name=ELMAT
*Elastic
1.,0.
*Material, name=RBMAT1
*Elastic
 3e+07,0.
*Material, name=RBMAT2
*Elastic
 3e+07,0.
**
** BOUNDARY CONDITIONS
**
** Name: Disp-BC-1 Type: Displacement/Rotation
*Boundary
LEFT, 1, 1
** Name: Disp-BC-2 Type: Displacement/Rotation
*Boundary
BOT, 2, 2
** Name: Disp-BC-3 Type: Displacement/Rotation
*Boundary
TOP, 2, 2
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, perturbation
*Static
**
** LOADS
**
** Name: DISTFORCE-1   Type: Pressure
*Dsload
_M8, P, -1000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*EL FILE,REBAR
 S,E,
*NODE FILE
 U,RF,
 COORD,
*EL PRINT,REBAR
 S,E,
*NODE PRINT
 U,RF,
 COORD,
*DLOAD
*End Step
** ----------------------------------------------------------------
**
** STEP: Step-2
**
*Step, name=Step-2, nlgeom
LARGEDISPLACEMENTANALYSIS
*Static
1., 1., 1e-05, 1.
**
** LOADS
**
** Name: DISTFORCE-2   Type: Pressure
*Dsload
_M9, P, -1000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-2
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-2
**
*Output, history, variable=PRESELECT
*EL FILE,REBAR
 S,E,
*NODE FILE
 U,RF,
 COORD,
*EL PRINT,REBAR
 S,E,
*NODE PRINT
 U,RF,
 COORD,
*DLOAD
*End Step