*HEADING : SIMPLE CONTACT TEST, FINITE SLIDING CONTACT WITHOUT FRICTION, RIGID ** Contact Features Tested: ** permeable-impermeable pore pressure contact for pore pressure coupled contact *NODE, NSET=BLOCK 1, 4., 1., 4. 2, 4., 1., 1. 3, 2., 1., 2. 4, 2., 1., 3. 5, 4., 3., 4. 6, 4., 3., 1. 7, 2., 3., 2. 8, 2., 3., 3. *NODE 9999, 0., 0., 0. *NSET,NSET=TOP 5,6,7,8 *NSET,NSET=BOT 1,2,3,4 *NSET,NSET=LEFT 3,4,7,8 *NSET,NSET=RIGHT 1,2,5,6 *ELEMENT, TYPE=C3D8RP, ELSET=BLOCK 1, 1,2,3,4,5,6,7,8 *SOLID SECTION, ELSET=BLOCK, MATERIAL=SOFT *HOURGLASS STIFFNESS 1.E7 *MATERIAL, NAME=SOFT *ELASTIC 30.E6, 0.3 *DENSITY 10., *PERMEABILITY,SPECIFIC=1.0 1.e-4, *INITIAL CONDITIONS,TYPE=RATIO BLOCK,1.0 *rigid body,analytical surface=BSURF, REFNODE=9999 *surface,TYPE=CYLINDER, NAME=BSURF 0., 0., 10., 10., 0., 10. 0., 0., -10. START, 0., 0. LINE, 10., 0. *surface,NAME=ASURF BLOCK,S1 *CONTACT PAIR,INTERACTION=SMOOTH ASURF,BSURF *SURFACE INTERACTION,NAME=SMOOTH *FRICTION 0.0, ** ** Step 1: Bring block into contact and push against rigid surface ** *STEP,AMP=RAMP *SOIL,CONSOLIDATION 0.1,1 *CONTROLS,PARAMETERS=FIELD 0.000001, *BOUNDARY 1, 1 2, 1 2, 3 9999, 1,6 TOP, 2,, -1.00001 TOP,8,8,1 *PRINT, CONTACT=YES *CONTACT PRINT,SECONDARY=ASURF *CONTACT FILE,SECONDARY=ASURF *EL FILE S, *NODE FILE,F=100 U, POR, *NODE PRINT U,POR *OUTPUT,FIELD *NODE OUTPUT U,POR *ELEMENT OUTPUT S, *CONTACT OUTPUT,VARIABLE=PRESELECT,SECONDARY=ASURF *END STEP ** ** Step 2: Apply normal load on top surface of block ** *STEP,AMP=RAMP *SOIL, CONSOLIDATION 0.1,1 *BOUNDARY,OP=NEW 1, 1 2, 1 2, 3 9999, 1,6 TOP,8,8,1 *DLOAD BLOCK, P2, 100.E3 *PRINT, CONTACT=YES *CONTACT FILE,SECONDARY=ASURF *EL FILE S, *NODE FILE,F=100 U,POR *NODE PRINT U,POR *END STEP ** ** Step 3: Slide block by fixing one end and pulling on the other ** *STEP,AMP=RAMP,NLGEOM *SOIL, CONSOLIDATION 0.1, 1. *BOUNDARY,OP=NEW LEFT,1,,-2.0 RIGHT,1 6,3 9999, 1,6 TOP,8,8,1 *CONTACT FILE,SECONDARY=ASURF *EL FILE S, *NODE FILE,F=100 U, *END STEP ** ** step 4: Steady state dynamics, direct analysis ** *STEP *STEADY STATE DYNAMICS,DIRECT 20,80,5 *BOUNDARY,OP=NEW 1, 1 2, 1 2, 3 9999, 1,6 TOP,8,8,1 *DLOAD BLOCK, P2, 100.E3 *NODE FILE U, RF, *EL FILE E, S, *CONTACT FILE *OUTPUT,FIELD *NODE OUTPUT U, RF, *ELEMENT OUTPUT E, S, *CONTACT OUTPUT,VARIABLE=PRESELECT,SECONDARY=ASURF *END STEP ** ** step 5: frequency extraction ** *STEP *FREQUENCY, eigensolver=lanczos, SIM=NO 17, , *BOUNDARY,OP=NEW 1, 1 2, 1 2, 3 9999, 1,6 TOP,8,8,1 *MODAL FILE *NODE FILE,F=0 *EL FILE,F=0 *NODE PRINT,F=0 *EL PRINT,F=0 *OUTPUT,FIELD,OP=NEW *NODE OUTPUT U, *CONTACT FILE,FREQ=0 *END STEP ** ** step 6: Steady state dynamics, subspace projection ** *STEP *STEADY STATE DYNAMICS,SUBSPACE PROJECTION,INTERVAL=RANGE 20,80,5 *DLOAD BLOCK, P2, 100.E3 *NODE FILE U, *EL FILE E, S, *OUTPUT,FIELD,OP=NEW *NODE OUTPUT U, *ELEMENT OUTPUT *CONTACT FILE *END STEP