*HEADING : TABULAR FREQUENCY DOMAIN VISCOELASTICITY, ELASTIC, C3D8 STEADY STATE DYNAMIC ANALYSIS OF CANTILEVER WITH DISTRIBUTED VERTICAL LOAD UNITS: SI *RESTART,WRITE *NODE,NSET=A 1, 6,,1. 11,,2. 16,,3. *NODE,NSET=B 5,10. 10,10.,1. 15,10.,2. 20,10.,3. *NFILL,NSET=SIDE A,B,4 *NCOPY,CHANGE NUMBER=100,OLD SET=SIDE,SHIFT ,,-1. *NSET,NSET=END,GENERATE 1,16,5 101,116,5 *ELEMENT,TYPE=C3D8 1,1,6,7,2,101,106,107,102 *ELGEN,ELSET=BEAM 1,4,,,3,5,4 *ELSET,ELSET=TOP,GENERATE 9,12 *SOLID SECTION,ELSET=BEAM,MATERIAL=VISCO *MATERIAL,NAME=VISCO *DENSITY 8000., **ELASTIC,MODULI=LONG TERM **200.E9,0.3 **VISCOELASTIC,FREQUENCY=TABULAR **1.775E-3,-5.116E-3,,,100.0 *USER MATERIAL,CONSTANTS=4 200.E9,0.3,1.775E-3,-5.116E-3 *BOUNDARY END,1,2 1,3,3 16,3,3 ** ******************************************* ** reference solution ** STEP1 *STEP,INC=500 *STEADY STATE DYNAMIC,DIRECT 100. *DLOAD TOP,P4,1.E9 *NODE PRINT,NSET=B U, RF, PU, PRF, *EL PRINT S, E, *ENERGY PRINT *OUTPUT,FIELD *NODE OUTPUT,NSET=B U, *OUTPUT,HISTORY *NODE OUTPUT,NSET=B U, *OUTPUT,FIELD *NODE OUTPUT,NSET=END RF, *OUTPUT,HISTORY *NODE OUTPUT, NSET=END RF, *OUTPUT,FIELD *ELEMENT OUTPUT S, E, *OUTPUT,HISTORY *ENERGY OUTPUT,VARIABLE=ALL *END STEP ***************************** **STEP 2 - extract all modes *STEP *FREQUENCY, eigensolver=lanczos, SIM=NO 102, , *NODE PRINT *EL PRINT *OUTPUT,FIELD *NODE OUTPUT *OUTPUT,FIELD *ELEMENT OUTPUT *END STEP ***************************** ** the subspace solution uses the entire eigenspace ** solution should be identical to the SSD,direct solution in the ** previous step ** STEP 3 *STEP *STEADY STATE DYNAMIC,SUBSPACE PROJECTION=ALL,INTERVAL=RANGE 100. *DLOAD TOP,P4,1.E9 *NODE PRINT,NSET=B U, RF, PU, PRF, *EL PRINT S, E, *ENERGY PRINT *OUTPUT,FIELD *NODE OUTPUT,NSET=B U, *OUTPUT,HISTORY *NODE OUTPUT,NSET=B U, *OUTPUT,FIELD *NODE OUTPUT,NSET=END RF, *OUTPUT,HISTORY *NODE OUTPUT, NSET=END RF, *OUTPUT,FIELD *ELEMENT OUTPUT S, E, *OUTPUT,HISTORY *ENERGY OUTPUT,VARIABLE=ALL *END STEP