*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, 7.5, 0. 1005, 7.5, 10. 2004, 5., 0. 2005, 5., 10. 3004, 2.5, 0. 3005, 2.5, 10. 4004, 10., 2.5 4005, 0., 2.5 5004, 10., 5. 5005, 0., 5. 6004, 10., 7.5 6005, 0., 7.5 *Element, type=CGAX4T 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 RB1LAYR1,0.040000,0.333300,0.000000,RBMAT1,90.000000,1 *ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-2 2001,2004,2005 *SURFACE SECTION,ELSET=SFMGAX1-2 *REBAR LAYER RB1LAYR2,0.040000,0.333300,0.000000,RBMAT1,90.000000,1 *ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-3 3001,3004,3005 *SURFACE SECTION,ELSET=SFMGAX1-3 *REBAR LAYER RB1LAYR3,0.040000,0.333300,0.000000,RBMAT1,90.000000,1 *ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-4 4001,4004,4005 *SURFACE SECTION,ELSET=SFMGAX1-4 *REBAR LAYER,GEOMETRY=ANGULAR RB2LAYR1,0.040000,46.245212,0.000000,RBMAT2,0.000000,1 *ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-5 5001,5004,5005 *SURFACE SECTION,ELSET=SFMGAX1-5 *REBAR LAYER,GEOMETRY=ANGULAR RB2LAYR2,0.040000,46.245212,0.000000,RBMAT2,0.000000,1 *ELEMENT,TYPE=SFMGAX1,ELSET=SFMGAX1-6 6001,6004,6005 *SURFACE SECTION,ELSET=SFMGAX1-6 *REBAR LAYER,GEOMETRY=ANGULAR RB2LAYR3,0.040000,44.568275,0.000000,RBMAT2,0.000000,1 *EMBEDDED ELEMENT 1001,2001,3001,4001,5001,6001 *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 *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 _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, unsymm=YES LARGEDISPLACEMENTANALYSIS *Coupled Temperature-Displacement, steady state 1., 1., *Solution Technique, type=SEPARATED ** ** 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