*HEADING : CONTACT TEST, RING SLIDING ON CYLINDER [ISL21A with CAXA41] Liner Perturbation steps with Load Case Definition *RESTART,WRITE,FREQ=99 *NODE 1, 1.3,7. 36, 1.3,0. 301, 1.6,7. 336, 1.6,0. 401, 1.6,8. 416, 1.6,6. 601, 1.8,8. 616, 1.8,6. 701, 1.8,7. 704, 1.8,6.4 1001, 2.1,7. 1004, 2.1,6.4 *NGEN,NSET=BASE 36,336,100 *NGEN,NSET=TOP 1,301,100 *NSET,NSET=BASEB,GENERATE 10036,10336,100 *NSET,NSET=TOPB,GENERATE 10001,10301,100 *NGEN,NSET=B1 401,601,100 *NGEN,NSET=B2 416,616,100 *NGEN,NSET=C1 701,1001,100 *NGEN,NSET=C2 704,1004,100 *NFILL TOP,BASE,35 B1,B2,15 C1,C2,3 *ELEMENT,TYPE=CAXA41,OFFSET=10000 1, 2,102,101,1 501, 402,502,501,401 801, 702,802,801,701 *ELGEN,ELSET=STEEL 1, 3,100,1, 35,1,10 501, 2,100,1, 15,1,10 801, 3,100,1, 3,1,10 *ELSET,ELSET=OUTER 803,813,823 *ELEMENT,TYPE=ISL21A 401, 401,402 701, 701,702 1401, 10401, 10402 1701, 10701, 10702 *ELGEN,ELSET=SLIDE1 401,15,1,1 *ELGEN,ELSET=SLIDE2 701,3,1,1 *ELGEN,ELSET=SLIDE1B 1401,15,1,1 *ELGEN,ELSET=SLIDE2B 1701,3,1,1 *INTERFACE,ELSET=SLIDE1 *FRICTION .2, *ASYMMETRIC-AXISYMMETRIC,MODE=1,ANGLE=0.0 *INTERFACE,ELSET=SLIDE2 *FRICTION .6, *ASYMMETRIC-AXISYMMETRIC,MODE=1,ANGLE=0.0 *INTERFACE,ELSET=SLIDE1B *FRICTION .2, *ASYMMETRIC-AXISYMMETRIC,MODE=1,ANGLE=180.0 *INTERFACE,ELSET=SLIDE2B *FRICTION .6, *ASYMMETRIC-AXISYMMETRIC,MODE=1,ANGLE=180.0 *SOLID SECTION,ELSET=STEEL,MATERIAL=STEEL *MATERIAL,NAME=STEEL *ELASTIC 30.E6,0.3 *SLIDE LINE,TYPE=LINEAR,ELSET=SLIDE1,GENERATE 301,331,1 *SLIDE LINE,TYPE=LINEAR,ELSET=SLIDE2,GENERATE 601,616,1 *SLIDE LINE,TYPE=LINEAR,ELSET=SLIDE1B,GENERATE 10301,10331,1 *SLIDE LINE,TYPE=LINEAR,ELSET=SLIDE2B,GENERATE 10601,10616,1 *NSET,NSET=NFILE 1, 36, 301, 336, 401, 416, 601, 616, 701, 704, 1001, 1004, 10001,10036,10301,10336,10401,10416,10601,10616,10701,10704,11001,11004, *ELSET,ELSET=EFILE1 409,410,411,412,413,701,702,703 1409,1410,1411,1412,1413,1701,1702,1703 *ELSET,ELSET=EFILE2 404,405,406,407,408,409,701,702,703 1404,1405,1406,1407,1408,1409,1701,1702,1703 ***ELSET,ELSET=EFILE ** SLIDE1,SLIDE2,SLIDE1B,SLIDE2B *STEP,NLGEOM PRESSURIZE COLLAR *STATIC 1.0,1.0 *BOUNDARY BASE,2 TOP,2 BASEB,2 TOPB,2 336,1 1001,2 601,2 10336,1 11001,2 10601,2 *DLOAD OUTER,P2,30000. *PRINT,CONTACT=YES *NODE PRINT,FREQ=2 U,RF *EL PRINT,ELSET=SLIDE1 S,E *EL PRINT,ELSET=SLIDE2 S,E *EL PRINT,ELSET=SLIDE1B S,E *EL PRINT,ELSET=SLIDE2B S,E *EL PRINT,ELSET=STEEL,FREQ=99 S, E, SINV, *OUTPUT,FIELD,FREQ=99 *ELEMENT OUTPUT,ELSET=EFILE1 S, *OUTPUT,FIELD,FREQ=99 *NODE OUTPUT,NSET=NFILE U,RF *END STEP *STEP,NLGEOM MOVE SLIDER DOWN *STATIC .1,1.0 *BOUNDARY BASE,2 TOP,2 336,1 1001,2,,-4.5 601,2,,-5. 10336,1 11001,2,,-4.5 10601,2,,-5. *OUTPUT,FIELD,FREQ=99 *ELEMENT OUTPUT,ELSET=EFILE2 S, *END STEP *STEP,PERTURBATION *STATIC *LOAD CASE,NAME="Slider Down-1" *BOUNDARY BASE,2 TOP,2 336,1 1001,2,,-2.25 601,2,,-2.5 *END LOAD CASE *LOAD CASE,NAME="Slider Down-2" *BOUNDARY BASE,2 TOP,2 336,1 1001,2,,-4.5 601,2,,-5 *END LOAD CASE *OUTPUT,FIELD,FREQ=99 *NODE OUTPUT,NSET=NFILE U,RF *END STEP