*HEADING A one element (CPS4R) input deck to test composite damage model Testing Model change *PREPRINT,ECHO=YES,HISTORY=YES **--------------------------------------------- Part1 *PART,NAME=PART-1 *NODE 1, 0.0, 0.0 4, 1.0, 0.0 13, 0.0, 1.0 16, 1.0, 1.0 *NGEN, NSET=BOT 1,4,1 *NGEN, NSET=TOP 13,16,1 *NFILL, NSET=NALL BOT, TOP, 3, 4 *ELEMENT,TYPE=CPS4R 1,1,2,6,5 *ELGEN, ELSET=EA 1, 3, 1, 1, 3, 4, 3 *SOLID SECTION,ELSET=EA,MATERIAL=GLASS_EPOXY,ORIENT=RECT 1., *NSET,NSET=Left 1,5,9,13 *nset, nset=right 4, 8, 12, 16 *ORIENTATION,NAME=RECT 1.0, 0.0, 0.0, 0.0, 1.0, 0.0 3,0.0 *END PART **--------------------------------------------- Assembly-1 *ASSEMBLY,NAME=ASSEMBLY-1 *INSTANCE,NAME=PART-1-1,PART=PART-1 *END INSTANCE *END ASSEMBLY **--------------------------------------------- End Assembly *MATERIAL,NAME=GLASS_EPOXY *ELASTIC,TYPE=LAMINA 53.8e9,17.9e9,0.25,8.96e9,8.96e9,6.88e9 **,,,,, *DAMAGE INITIATION,CRITERION=HASHIN,ALPHA=0.0 1034e6,1034e6,27.6e6,138e6,41.4e6,50e6 ** ,,,,, *DAMAGE EVOLUTION, TYPE=ENERGY, SOFTENING=LINEAR 10e6,10e6,5e6,5e6 *DAMAGE STABILIZATION 0.0001, 0.0001, 0.0001, 0.0001 *STEP,INC=200,nlgeom *STATIC 0.001,0.01,,0.001 *BOUNDARY ASSEMBLY-1.PART-1-1.right,1,1,0.001 ASSEMBLY-1.PART-1-1.left,1,1 ASSEMBLY-1.PART-1-1.bot, 2,2 *ENERGY PRINT *NODE PRINT U, *OUTPUT,FIELD *ELEMENT OUTPUT DMICRT S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT U,RF *OUTPUT,HISTORY *ELEMENT OUTPUT,ELSET=PART-1-1.EA HSNFTCRT, HSNFCCRT, HSNMTCRT, HSNMCCRT, S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT,NSET=PART-1-1.right RF, U *EL PRINT HSNFTCRT *END STEP *************************************** *STEP,INC=200,nlgeom *STATIC 0.01,0.01,,0.001 *MODEL CHANGE, TYPE=ELEMENT, REMOVE PART-1-1.5, *ENERGY PRINT *NODE PRINT U, *OUTPUT,FIELD *ELEMENT OUTPUT DMICRT S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT U,RF *OUTPUT,HISTORY *ELEMENT OUTPUT,ELSET=PART-1-1.EA HSNFTCRT, HSNFCCRT, HSNMTCRT, HSNMCCRT, S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT,NSET=PART-1-1.right RF, U *EL PRINT HSNFTCRT *END STEP **************************************************** *STEP,INC=200,nlgeom *STATIC 0.001,0.01,,0.001 *BOUNDARY ASSEMBLY-1.PART-1-1.right,1,1,0.1 *ENERGY PRINT *NODE PRINT U, *OUTPUT,FIELD *ELEMENT OUTPUT DMICRT S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT U,RF *OUTPUT,HISTORY *ELEMENT OUTPUT,ELSET=PART-1-1.EA HSNFTCRT, HSNFCCRT, HSNMTCRT, HSNMCCRT, S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT,NSET=PART-1-1.right RF, U *EL PRINT HSNFTCRT *END STEP ****************************REACTIVATION***************** *STEP,INC=200,nlgeom *STATIC 0.01,0.01,,0.001 *MODEL CHANGE, TYPE=ELEMENT, ADD=STRAIN FREE PART-1-1.5, *ENERGY PRINT *NODE PRINT U, *OUTPUT,FIELD *ELEMENT OUTPUT DMICRT S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT U,RF *OUTPUT,HISTORY *ELEMENT OUTPUT,ELSET=PART-1-1.EA HSNFTCRT, HSNFCCRT, HSNMTCRT, HSNMCCRT, S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT,NSET=PART-1-1.right RF, U *EL PRINT HSNFTCRT *END STEP **************************************************** *STEP,INC=200,nlgeom *STATIC 0.001,0.01,,0.001 *BOUNDARY ASSEMBLY-1.PART-1-1.right,1,1,0.2 *ENERGY PRINT *NODE PRINT U, *OUTPUT,FIELD *ELEMENT OUTPUT DMICRT S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT U,RF *OUTPUT,HISTORY *ELEMENT OUTPUT,ELSET=PART-1-1.EA HSNFTCRT, HSNFCCRT, HSNMTCRT, HSNMCCRT, S, E, DAMAGEFT, DAMAGEFC, DAMAGEMT, DAMAGEMC, DAMAGESHR, STATUS, *NODE OUTPUT,NSET=PART-1-1.right RF, U *EL PRINT HSNFTCRT *END STEP ****************************REACTIVATION*****************