*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=C3D20
*Elset, elset=SLAB1, generate
*Elset, elset=SLAB, generate
** Region: (Section-1-SLAB:SLAB)
*Elset, elset=_I1, internal, generate
** Section: Section-1-SLAB
*Solid Section, elset=_I1, material=A1
1.,
*ORIENTATION,NAME=REBAR1,DEFINITION=OFFSET TO NODES
*ELEMENT,TYPE=SFM3D8R,ELSET=SFM3D8R-1
*SURFACE SECTION,ELSET=SFM3D8R-1
*REBAR LAYER,ORIENTATION=REBAR1
RE,0.193320,18.000000,0.000000,A2,90.000000,1
*EMBEDDED ELEMENT
*End Instance
*Nset, nset=EDGE1, instance=PART-1-1, generate
*Nset, nset=END2, instance=PART-1-1, generate
*Nset, nset=END3, instance=PART-1-1, generate
*Nset, nset=ROLLER, instance=PART-1-1, generate
*Nset, nset=X-SYM, instance=PART-1-1, generate
*Nset, nset=X-SYM1, instance=PART-1-1, generate
*Nset, nset=X-SYM2, instance=PART-1-1, generate
*Elset, elset=MID, instance=PART-1-1
*Nset, nset=_M11, internal, instance=PART-1-1
*End Assembly
**
** MATERIALS
**
*Material, name=A1
*Concrete
*Failure Ratios
*Tension Stiffening
*Elastic
 4.2e+06, 0.18
*Material, name=A2
*Elastic
 2.9e+07,0.
*Plastic
31900.,0.
**
** BOUNDARY CONDITIONS
**
** Name: Disp-BC-1 Type: Symmetry/Antisymmetry/Encastre
*Boundary
X-SYM, XSYMM
** Name: Disp-BC-2 Type: Displacement/Rotation
*Boundary
ROLLER, 2, 2
** Name: Disp-BC-3 Type: Displacement/Rotation
*Boundary
_M11, 3, 3
*STEP,INC=30
*STATIC,RIKS
0.05,  1.0,  .001,  ,  ,  PART-1-1.141,  2,  -.4
*CLOAD
PART-1-1.87,2,-1666.66667
PART-1-1.187,2,-6666.66667
PART-1-1.287,2,-1666.66667
*EL PRINT,ELSET=MID,FREQUENCY=5
S,
E,
SINV,
PE,
*EL PRINT,ELSET=MID,FREQUENCY=1,REBAR
S,E
PE,
*EL PRINT,ELSET=PART-1-1.SLAB
CRACK,
CONF,
*NODE FILE,NSET=X-SYM
U,
CF,
RF,
*OUTPUT,FIELD
*NODE OUTPUT,NSET=X-SYM
U,
CF,
RF,
*EL FILE, REBAR, F=1
S,
E,
*CONTROLS,PARAMETERS=FIELD
2.e-3,
*END STEP