*HEADING : EXPONENTIAL DECAY FRICTION (1 SLIP DIR, LAGRANGE MULTIPLIER) *RESTART,WRITE,FREQ=0 *NODE, NSET=NALL 1, 0., 0. 2, 0., 1. 3, 1., 0. 4, 1., 1. 100, 0., 0. *ELEMENT,TYPE=B21,ELSET=BEAM 1, 1,2 2, 3,4 *BEAM SECTION,SECT=CIRC,ELSET=BEAM,MATERIAL=ELAS,TEMP=GRADIENTS 0.564189584, 0.,0.,-1., *MATERIAL,NAME=ELAS *ELASTIC 30.E6,0.3 *rigid body,analytical surface=RS1,REFNODE=100 *surface,TYPE=SEGMENTS,NAME=RS1 START,-10.,0. LINE,10.,0. *surface,type=node,NAME=CN1 1, *surface,type=node,NAME=CN2 3, *CONTACT PAIR,INTERACTION=CI1 CN1,RS1 *CONTACT PAIR,INTERACTION=CI2 CN2,RS1 *SURFACE INTERACTION,NAME=CI1 1.0, *FRICTION, EXPONENTIAL DECAY, LAGRANGE 0.3, 0.1, 4.0 *GAP CONDUCTANCE 10.0,0. 10.0,1. *SURFACE INTERACTION,NAME=CI2 1.0, *FRICTION, ROUGH *AMPLITUDE,NAME=AMP1 0.0, 0.0, 0.2, 0.0625, 0.4, 0.1250, 0.6, 0.2500, 0.8, 0.5, 1.0, 1.0 ** ** STEP 1: ESTABLISH CONTACT (PRESCRIBED DISPLACEMENT) ** *STEP, NLGEOM ESTABLISH CONTACT (PRECRIBED DISPLACEMENT) *STATIC 1.,1. *BOUNDARY 100,1,2,0.0 100,6,6,0.0 2,1,1,0.0 2,2,2,-1.e-5 2,6,6,0.0 4,1,1,0.0 4,2,2,-1.e-5 4,6,6,0.0 *NODE PRINT, FREQ=0 *OUTPUT,FIELD,FREQ=0 *NODE OUTPUT *EL PRINT, FREQ=0 *OUTPUT,FIELD,FREQ=0 *ELEMENT OUTPUT *PRINT,CONTACT=YES *OUTPUT,FIELD,FREQ=0 *CONTACT OUTPUT,VARIABLE=PRESELECT,SLAVE=CN1,MASTER=RS1 *OUTPUT,FIELD,FREQ=0 *CONTACT OUTPUT,VARIABLE=PRESELECT,SLAVE=CN2,MASTER=RS1 *CONTACT PRINT, F=0, SLAVE=CN1, MASTER=RS1 *CONTACT PRINT, F=0, SLAVE=CN2, MASTER=RS1 *END STEP ** ** STEP 2: ESTABLISH CONTACT (APPLY NORMAL PRESSURE = 300) ** *STEP, NLGEOM ESTABLISH CONTACT (APPLY NORMAL PRESSURE = 300) *STATIC 1.,1. *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,1,1,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD 2,2,-300.0 4,2,-300.0 *END STEP ** ** STEP 3: APPLY SHEAR FORCE (Teq < Tcrit) ** ** Given: P=300.0, Tau=85.0 ** Results: mu=0.3 ** Tcrit=90 --> "Sticking" ** *STEP, NLGEOM APPLY SHEAR FORCE (Teq < Tcrit) *STATIC .1,1. *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,1,85.0 2,2,-300.0 4,2,-300.0 *OUTPUT,FIELD,FREQ=1 *CONTACT OUTPUT,VARIABLE=PRESELECT,SLAVE=CN1,MASTER=RS1 CSTRESS,CDISP *CONTACT PRINT, F=99, SLAVE=CN1, MASTER=RS1 *PRINT,CONTACT=YES *END STEP ** ** STEP 4: REMOVE SHEAR FORCES ** *STEP, NLGEOM REMOVE SHEAR FORCES *STATIC .1,1. *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,2,-300.0 4,2,-300.0 *END STEP ** ** STEP 5: CHANGE FRICTION AND APPLY SHEAR FORCE ** ** Given: P=300.0, Tau=-145.0 ** Results: mu=0.5, Tcrit=150.0 "sticking" ** *STEP, NLGEOM CHANGE FRICTION TO AN ISOTROPIC MODEL *STATIC .1,1.0 *CHANGE FRICTION, INTERACTION=CI1 *FRICTION, EXPONENTIAL DECAY, TEST DATA, LAGRANGE 0.5, 0.3, 0.2 0.2, *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,1,-145.0 2,2,-300.0 4,2,-300.0 *END STEP ** ** STEP 6: REMOVE SHEAR FORCES ** *STEP, NLGEOM REMOVE SHEAR FORCES (2) *STATIC .1,1.0 *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,2,-300.0 4,2,-300.0 *END STEP ** ** STEP 7: RESET THE FRICTION MODEL TO THE ORIGINAL MODEL ** AND APPLY A SLIP ** *STEP, NLGEOM RESET THE FRICTION MODEL TO THE ORIGINAL MODEL *STATIC .1,1.0 *CHANGE FRICTION, RESET, INTERACTION=CI1 *BOUNDARY,OP=NEW 100,1,2,0.0 100,6,6,0.0 2,6,6,0.0 2,1,1,0.2 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,2,-300.0 4,2,-300.0 *END STEP ** ** STEP 8: CHANGE FRICTION FOR ROD 2 ** *STEP, NLGEOM, AMP=STEP CHANGE FRICTION FOR ROD 2 *STATIC ,1.0 *CHANGE FRICTION, INTERACTION=CI1 *FRICTION, LAGRANGE 0.0, *CHANGE FRICTION, INTERACTION=CI2 *FRICTION, EXPONENTIAL DECAY, TEST DATA, LAGRANGE 0.3, 0.0 0.1, 0.2 *BOUNDARY, OP=NEW 100,1,2,0.0 100,6,6,0.0 2,1,1,0.0 2,6,6,0.0 4,1,1,0.0 4,6,6,0.0 *CLOAD, OP=NEW 2,2,-300.0 4,2,-300.0 *CONTACT PRINT, F=0, SLAVE=CN2, MASTER=RS1 *OUTPUT,FIELD,FREQ=0 *CONTACT OUTPUT,VARIABLE=PRESELECT,SLAVE=CN2,MASTER=RS1 *END STEP ** ** STEP 9: APPLY A SLIP ON ROD 2 ** *STEP, NLGEOM APPLY SLIP ON ROD 2 *STATIC .1,1.0 *BOUNDARY, OP=MOD, AMP=AMP1 4,1,1,1.0 *CONTACT PRINT, F=99, SLAVE=CN2, MASTER=RS1 *OUTPUT,FIELD,FREQ=1 *CONTACT OUTPUT,VARIABLE=PRESELECT,SLAVE=CN2,MASTER=RS1 CSTRESS,CDISP *END STEP