*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.
      5,           5.,           0.
      6,          10.,           5.
      7,           5.,          10.
      8,           0.,           5.
   1008,          10.,          2.5
   1009,           5.,          2.5
   1010,           0.,          2.5
   2008,          10.,           5.
   2009,           5.,           5.
   2010,           0.,           5.
   3008,          10.,          7.5
   3009,           5.,          7.5
   3010,           0.,          7.5
*Element, type=CGAX8T
1, 1, 2, 3, 4, 5, 6, 7, 8
*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
*MPC
LINEAR,6,2,3
LINEAR,5,1,2
LINEAR,7,4,3
LINEAR,8,1,4
*ELEMENT,TYPE=SFMGAX2,ELSET=SFMGAX2-1
1001,1008,1009,1010
*SURFACE SECTION,ELSET=SFMGAX2-1
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR1,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMGAX2,ELSET=SFMGAX2-2
2001,2008,2009,2010
*SURFACE SECTION,ELSET=SFMGAX2-2
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR2,0.040000,46.245212,0.000000,RBMAT1,0.000000,1
*ELEMENT,TYPE=SFMGAX2,ELSET=SFMGAX2-3
3001,3008,3009,3010
*SURFACE SECTION,ELSET=SFMGAX2-3
*REBAR LAYER,GEOMETRY=ANGULAR
RB1LAYR3,0.040000,46.245212,0.000000,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, 5
*Nset, nset=LEFT, instance=PART-1-1
 1, 4, 8
*Nset, nset=TOP, instance=PART-1-1
 3, 4, 7
*Elset, elset=__M6_S2, internal, instance=PART-1-1
 1,
*Surface, type=ELEMENT, name=_M6, internal
__M6_S2, S2
*Elset, elset=__M7_S2, internal, instance=PART-1-1
 1,
*Surface, type=ELEMENT, name=_M7, internal
__M7_S2, S2
*End Assembly
** 
** MATERIALS
** 
*Material, name=ELMAT
*Conductivity
1.,
*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
_M6, 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 Print, freq=999999
*Node Print, freq=999999
*EL FILE, F=1
S,
E,
*EL FILE, REBAR, F=1
S,
E,
*NODE FILE, F=1
U,
RF,
*End Step
** ----------------------------------------------------------------
** 
** STEP: Step-2
** 
*Step, name=Step-2, nlgeom
LARGEDISPLACEMENTANALYSIS
*Coupled Temperature-Displacement, steady state
1., 1., 
** 
** LOADS
** 
** Name: DISTFORCE-2   Type: Pressure
*Dsload
_M7, P, -1000.
** 
** OUTPUT REQUESTS
** 
*Restart, write, frequency=0
** 
** FIELD OUTPUT: F-Output-2
** 
*Output, field
*Element Output, Rebar, variable=preselect
S,
E,
*node output, variable=preselect
** 
** HISTORY OUTPUT: H-Output-2
** 
*Output, history, variable=PRESELECT
*EL FILE, F=1
S,
E,
*EL FILE, REBAR, F=1
S,
E,
*NODE FILE, F=1
U,
RF,
*End Step