*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., -0.75 2, 1.5, -0.75 3, 3., -0.75 4, 4.5, -0.75 5, 6., -0.75 6, 7.5, -0.75 7, 9., -0.75 8, 10.5, -0.75 9, 12., -0.75 10, 13.5, -0.75 11, 15., -0.75 21, 0., -0.375 22, 1.5, -0.375 23, 3., -0.375 24, 4.5, -0.375 25, 6., -0.375 26, 7.5, -0.375 27, 9., -0.375 28, 10.5, -0.375 29, 12., -0.375 30, 13.5, -0.375 31, 15., -0.375 41, 0., 0. 42, 1.5, 0. 43, 3., 0. 44, 4.5, 0. 45, 6., 0. 46, 7.5, 0. 47, 9., 0. 48, 10.5, 0. 49, 12., 0. 50, 13.5, 0. 51, 15., 0. 61, 0., 0.375 62, 1.5, 0.375 63, 3., 0.375 64, 4.5, 0.375 65, 6., 0.375 66, 7.5, 0.375 67, 9., 0.375 68, 10.5, 0.375 69, 12., 0.375 70, 13.5, 0.375 71, 15., 0.375 81, 0., 0.75 82, 1.5, 0.75 83, 3., 0.75 84, 4.5, 0.75 85, 6., 0.75 86, 7.5, 0.75 87, 9., 0.75 88, 10.5, 0.75 89, 12., 0.75 90, 13.5, 0.75 91, 15., 0.75 *Element, type=CPS8 1, 1, 3, 43, 41, 2, 23, 42, 21 2, 41, 43, 83, 81, 42, 63, 82, 61 3, 3, 5, 45, 43, 4, 25, 44, 23 4, 43, 45, 85, 83, 44, 65, 84, 63 5, 5, 7, 47, 45, 6, 27, 46, 25 6, 45, 47, 87, 85, 46, 67, 86, 65 7, 7, 9, 49, 47, 8, 29, 48, 27 8, 47, 49, 89, 87, 48, 69, 88, 67 9, 9, 11, 51, 49, 10, 31, 50, 29 10, 49, 51, 91, 89, 50, 71, 90, 69 *Elset, elset=SLAB, generate 1, 10, 1 *Elset, elset=SLAB1, generate 1, 9, 2 ** Region: (Section-1-SLAB:SLAB) *Elset, elset=_I1, internal, generate 1, 10, 1 ** Section: Section-1-SLAB *Solid Section, elset=_I1, material=A1 18., *ORIENTATION,NAME=REBAR1,DEFINITION=OFFSET TO NODES 2,4 3 *REBAR,ELEMENT=CONTINUUM,GEOMETRY=ISOPARAMETRIC,MATERIAL=A2,NAME=REB SLAB1, .19332,18. , 0., .62666667, 3 *End Instance *Nset, nset=END1, instance=PART-1-1, generate 1, 81, 20 *Nset, nset=END2, instance=PART-1-1, generate 11, 91, 20 *Nset, nset=ROLLER, instance=PART-1-1 11, *Nset, nset=X-SYM, instance=PART-1-1, generate 1, 81, 20 *Elset, elset=MID, instance=PART-1-1 1, 2 *Elset, elset=SLAB2, instance=PART-1-1, generate 2, 10, 2 *End Assembly ** ** MATERIALS ** *Material, name=A1 *Concrete 2670., 0. 4640., 0.0013 *Failure Ratios 1.16, 0.0625, 1.28, 0.3333 *Tension Stiffening 1., 0. 0., 0.0005 *Elastic 4.2e+06, 0.18 *Material, name=A2 *Elastic 2.9e+07,0. *Plastic 31900.,0. ** ** BOUNDARY CONDITIONS ** ** Name: Disp-BC-1 Type: Displacement/Rotation *Boundary X-SYM, 1, 1 ** Name: Disp-BC-2 Type: Displacement/Rotation *Boundary ROLLER, 2, 2 *RESTART,WRITE,FREQUENCY=5 *STEP,INC=30 *STATIC,RIKS .05 , 1. , , , , PART-1-1.41, 2, -.3 *CLOAD PART-1-1.87,2,-10000. *NODE FILE,NSET=X-SYM U, CF, RF, *OUTPUT,FIELD *Element Output, Rebar S, E, *Element Output S, E, *NODE OUTPUT,NSET=X-SYM U, CF, RF, *EL FILE, REBAR, F=1 S, E, *END STEP