*HEADING QUASI-STATIC TEST OF SHELL TO SOLID COUPLING *PREPRINT, MODEL=YES ** JOB NAME: XSHELL2SOLID_S4R_C3D8_XPL MODEL NAME: MODEL-1 ** ** PARTS ** *PART, NAME=PART-1 *END PART *PART, NAME=PART-2 *END PART ** ** ASSEMBLY ** *ASSEMBLY, NAME=ASSEMBLY ** *INSTANCE, NAME=PART-1-1, PART=PART-1 0., -3.06151588455594E-17, -2.22044604925031E-16 0., -3.06151588455594E-17, -2.22044604925031E-16, 0., -1., -2.22044604925031E-16, 90. *NODE, NSET=NALL 1, -0.5, 0.125, 0. 2, -0.5, -0.125, 0. 3, -0.5, 0.125, 2. 4, -0.5, -0.125, 2. 5, 0., 0.125, 0. 6, 0., -0.125, 0. 7, 0., 0.125, 2. 8, 0., -0.125, 2. 9, 0.5, 0.125, 0. 10, 0.5, -0.125, 0. 11, 0.5, 0.125, 2. 12, 0.5, -0.125, 2. *NSET, NSET=QA_TEST1 3,7,11, *ELEMENT, TYPE=C3D8R 1, 5, 6, 8, 7, 1, 2, 4, 3 2, 9, 10, 12, 11, 5, 6, 8, 7 ** REGION: (SECTION-1:PICKED) *ELSET, ELSET=_I1, INTERNAL 1, 2 ** SECTION: SECTION-1 *SOLID SECTION, ELSET=_I1, MATERIAL=MATERIAL-1 1., *END INSTANCE ** *INSTANCE, NAME=PART-2-1, PART=PART-2 0., 0., 0. 0., 0., 0., 1., 0., 0., 90. *NODE, NSET=NALL 1, 0., 0., 0. 2, 8., 0., 0. 3, 8., 0.5, 0. 4, 0., 0.5, 0. 5, 0., -0.5, 0. 6, 8., -0.5, 0. 7, 2., 0., 0. 8, 4., 0., 0. 9, 6., 0., 0. 10, 6., 0.5, 0. 11, 4., 0.5, 0. 12, 2., 0.5, 0. 13, 2., -0.5, 0. 14, 4., -0.5, 0. 15, 6., -0.5, 0. *NSET, NSET=QA_TEST2 1,4,5, *ELEMENT, TYPE=S4R 1, 1, 7, 12, 4 2, 7, 8, 11, 12 3, 8, 9, 10, 11 4, 9, 2, 3, 10 5, 2, 9, 15, 6 6, 9, 8, 14, 15 7, 8, 7, 13, 14 8, 7, 1, 5, 13 ** REGION: (SECTION-2:PICKED) *ELSET, ELSET=_I1, INTERNAL, GENERATE 1, 8, 1 ** SECTION: SECTION-2 *SHELL SECTION, ELSET=_I1, MATERIAL=MATERIAL-1 0.25, 3 *END INSTANCE *NSET, NSET=_G9, INTERNAL, INSTANCE=PART-1-1 3, 4, 7, 8, 11, 12 *ELSET, ELSET=_G9, INTERNAL, INSTANCE=PART-1-1 1, 2 *NSET, NSET=_G10, INTERNAL, INSTANCE=PART-2-1 3, 6 *NSET, NSET=_G11, INTERNAL, INSTANCE=PART-2-1 2, *NSET, NSET=_G12, INTERNAL, INSTANCE=PART-2-1 3, 6 *NSET, NSET=_G13, INTERNAL, INSTANCE=PART-2-1 2, *NSET, NSET=_G14, INTERNAL, INSTANCE=PART-2-1 3, 6 *NSET, NSET=_G15, INTERNAL, INSTANCE=PART-2-1 2, *NSET, NSET=_G16, INTERNAL, INSTANCE=PART-2-1 3, 6 *NSET, NSET=_G17, INTERNAL, INSTANCE=PART-2-1 2, *NSET, NSET=_G18, INTERNAL, INSTANCE=PART-1-1 3, 4, 7, 8, 11, 12 *ELSET, ELSET=_G18, INTERNAL, INSTANCE=PART-1-1 1, 2 *NSET, NSET=_G19, INTERNAL, INSTANCE=PART-1-1 3, 4, 7, 8, 11, 12 *ELSET, ELSET=_G19, INTERNAL, INSTANCE=PART-1-1 1, 2 *NSET, NSET=_G20, INTERNAL, INSTANCE=PART-2-1 2, 3, 6 *ELSET, ELSET=_G20, INTERNAL, INSTANCE=PART-2-1 4, 5 *ELSET, ELSET=_SURF-1_S3, INTERNAL, INSTANCE=PART-1-1 1, 2 *SURFACE, TYPE=ELEMENT, NAME=SURF-1 _SURF-1_S3, S3 *ELSET, ELSET=_SURF-2_E4, INTERNAL, INSTANCE=PART-2-1 1, *ELSET, ELSET=_SURF-2_E2, INTERNAL, INSTANCE=PART-2-1 8, *SURFACE, TYPE=ELEMENT, NAME=SURF-2 _SURF-2_E4, E4 _SURF-2_E2, E2 ** CONSTRAINT: CONSTRAINT-1 *SHELL TO SOLID COUPLING, CONSTRAINT NAME=CONSTRAINT-1,INFLUENCE DISTANCE=.125 SURF-2, SURF-1 *END ASSEMBLY ** ** MATERIALS ** *MATERIAL, NAME=MATERIAL-1 *DENSITY .5, *ELASTIC 3E+07, 0.3 *AMPLITUDE, NAME=AMP1,DEFINITION=SMOOTH STEP 0.0,0.0,1.,1.0 *AMPLITUDE, NAME=AMP2,DEFINITION=SMOOTH STEP 0.0,1.0,1.,0.0 *NSET, NSET=QA_TEST ASSEMBLY.PART-1-1.QA_TEST1, ASSEMBLY.PART-2-1.QA_TEST2 ** ** STEP: STEP-1 ** *STEP, NAME=STEP-1, NLGEOM=YES BEND - NONLINEAR *DYNAMIC, EXPLICIT , 1., ** ** BOUNDARY CONDITIONS ** ** NAME: BC-3 TYPE: DISPLACEMENT/ROTATION *BOUNDARY _G19, 1, 1 _G19, 2, 2 _G19, 3, 3 ** ** LOADS ** ** NAME: LOAD-5 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP1 _G14, 2, -15. ** NAME: LOAD-6 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP1 _G15, 2, -30. ** ** OUTPUT REQUESTS ** *RESTART, WRITE, NUMBER=1 ** ** FIELD OUTPUT: F-OUTPUT-2 ** *OUTPUT, FIELD, NUMBER INTERVAL=4 *NODE OUTPUT, NSET=QA_TEST U, ***ELEMENT OUTPUT ***S, ** ** HISTORY OUTPUT: H-OUTPUT-2 ** *OUTPUT, HISTORY, VARIABLE=PRESELECT *END STEP ** ---------------------------------------------------------------- ** ** STEP: STEP-2 ** *STEP, NAME=STEP-2, NLGEOM=YES PULL - NONLINEAR *DYNAMIC, EXPLICIT ,1., ** ** LOADS ** ** NAME: LOAD-7 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP1 _G16, 1, 15. ** NAME: LOAD-8 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP1 _G17, 1, 30. *END STEP ** ---------------------------------------------------------------- ** ** STEP: STEP-3 ** *STEP, NAME=STEP-3, NLGEOM=YES UNLOAD *DYNAMIC, EXPLICIT , 1., ** ** LOADS ** ** NAME: LOAD-7 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP2 _G16, 1, 15. ** NAME: LOAD-8 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP2 _G17, 1, 30. ** NAME: LOAD-5 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP2 _G14, 2, -15. ** NAME: LOAD-6 TYPE: CONCENTRATED FORCE *CLOAD, AMPLITUDE=AMP2 _G15, 2, -30. *END STEP ** ---------------------------------------------------------------- ** ** STEP: STEP-4 ** *STEP, NAME=STEP-4, NLGEOM=YES RIGID ROTATION *DYNAMIC,EXPLICIT , 1., ** ** BOUNDARY CONDITIONS ** ** NAME: BC-3 TYPE: DISPLACEMENT/ROTATION *BOUNDARY, OP=NEW ** NAME: BC-4 TYPE: DISPLACEMENT/ROTATION *BOUNDARY, OP=NEW, AMPLITUDE=AMP1 _G20, 1, 1 _G20, 2, 2 _G20, 3, 3 _G20, 6, 6, -1.5708 *END STEP