*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
      1,           0.,           0.
      2,          10.,           0.
      3,          10.,          10.
      4,           0.,          10.
   1004,          10.,          2.5
   1005,           0.,          2.5
   2004,          10.,           5.
   2005,           0.,           5.
   3004,          10.,          7.5
   3005,           0.,          7.5
*Element, type=CGAX4
1, 1, 2, 3, 4
*Elset, elset=AXSOL
 1,
** Region: (Section-1-AXSOL:AXSOL)
*Elset, elset=_I1, internal
 1,
** Section: Section-1-AXSOL
*Solid Section, elset=_I1, material=ELMAT
1.,
*ORIENTATION,NAME=REBAR1,DEFINITION=OFFSET TO NODES
2,4
3
*ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-1
1001,1004,1005
*SURFACE SECTION,ELSET=SFMGAX1-1
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR1,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-2
2001,2004,2005
*SURFACE SECTION,ELSET=SFMGAX1-2
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR2,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-3
3001,3004,3005
*SURFACE SECTION,ELSET=SFMGAX1-3
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR3,0.040000,44.568275,0.000000,RBMAT1,0.000000,1
*EMBEDDED ELEMENT
1001,2001,3001
*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
 1, 2
*Nset, nset=LEFT, instance=PART-1-1
 1, 4
*Nset, nset=TOP, instance=PART-1-1
 3, 4
*Nset, nset=EqnSet-1, instance=PART-1-1
 3,
*Nset, nset=EqnSet-2, instance=PART-1-1
 2,
*Elset, elset=__M8_S2, internal, instance=PART-1-1
 1,
*Surface, type=ELEMENT, name=_M8, internal
__M8_S2, S2
*Elset, elset=__M9_S2, internal, instance=PART-1-1
 1,
*Surface, type=ELEMENT, name=_M9, internal
__M9_S2, S2
*Equation
2
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
BOT, 3, 3
BOT, 4, 4
BOT, 5, 5
** 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,
*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,
*End Step