*HEADING ** ** ABAQUS INPUT FILE UPGRADE: This input file was upgraded from ** version 5.8 or later to version 6.3 with 0 warning(s) and 0 ** error(s). ** ** : RANDOM RESPONSE PROCEDURE FOR BASE MOTION ** ** THIS INPUT FILE TESTS ** 1) CORRELATED AND UNCORRELATED LOADINGS FOR ** BASE MOTION ** 2) LOAD CASE NUMBERING ** ** PROBLEM: CANTILEVER BEAM ** 1) TWO B21 ELEMENTS OF UNIT LENGTH ALIGNED VERTICALLY ** 2) BASE MOTION APPLIED TO GLOBAL DOFS 1 AND 6 ** 3) WHITE NOISE POWER SPECTRAL DENSITY INPUT ** 4) TWO MODE SHAPES USED IN RANDOM RESPONSE ** ** RESULTS: AGREE WITH HAND CALCULATIONS ** 1) RESULTS FROM STEP 2 AND STEP 4 SHOULD BE THE SAME ** (TESTS LOAD CASE NUMBERING) ** 2) RESULTS FROM STEP 3 AND STEP 5 SHOULD BE THE SAME ** (TESTS LOAD CASE NUMBERING) ** *NODE,NSET=ALL 10,0., 0.,0. 20,0.,10.,0. 30,0.,20.,0. *transform, nset=all 1., 1., 0., -1., 1., 0. *ELEMENT,ELSET=ALL,TYPE=B21 10,10,20 20,20,30 *BEAM SECTION,SECTION=RECT,ELSET=ALL,MATERIAL=STEEL 1.,1. *MATERIAL,NAME=STEEL *ELASTIC 30.E6,0.3 *DENSITY 0.283, *BOUNDARY 10,ENCASTRE *PSD-DEFINITION,NAME=WHITE,TYPE=BASE 1.0E+2,0.,0. 1.0E+2,0.,3000. *STEP *** STEP 1: FREQUENCY STEP *** *FREQUENCY, eigensolver=lanczos 2, , *NODE PRINT,FREQ=1 U, *EL PRINT,FREQ=0 *NODE FILE,FREQ=0 *EL FILE,FREQ=0 *MODAL FILE *ENDSTEP *STEP *** STEP 2: CORRELATED CLOADS *** *RANDOM RESPONSE 1,25,10,5,1 *modal damping, modal=direct 1,2,0.01 *select eigenmodes, generate 1, 2 *CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=CORRELATED 1,1.,1. *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1,DOF=1 *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1,DOF=6 ** *EL PRINT,FREQ=10 S, SF, *EL FILE,ELSET=ALL S, SF, *NODE PRINT,NSET=ALL,FREQ=10 U, TU, RTU, *NODE PRINT,NSET=ALL,FREQ=10,GLOBAL=YES U, TU, RTU, *NODE FILE,NSET=ALL U, TU, RTU *OUTPUT,FIELD,VAR=PRESELECT *ENDSTEP *STEP *** STEP 3: UNCORRELATED *** *RANDOM RESPONSE 1,25,10,5,1 *modal damping, modal=direct 1,2,0.01 *select eigenmodes, generate 1, 2 *CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=UNCORRELATED 2,1.,1. *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2,DOF=1 *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2,DOF=6 ** *EL PRINT,FREQ=10 S, SF, *EL FILE,ELSET=ALL S, SF, *NODE PRINT,NSET=ALL,FREQ=10 U, TU, RTU, *NODE PRINT,NSET=ALL,FREQ=10,GLOBAL=YES U, TU, RTU, *NODE FILE,NSET=ALL U, TU, RTU *ENDSTEP *STEP *** STEP 4: CORRELATED WITH DIFFERENT LOAD CASE NUMBER *** *RANDOM RESPONSE 1,25,10,5,1 *modal damping, modal=direct 1,2,0.01 *select eigenmodes, generate 1, 2 *CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=CORRELATED 1000,1.,1. *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1000,DOF=1 *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1000,DOF=6 ** *EL PRINT,FREQ=10 S, SF, *EL FILE,ELSET=ALL S, SF, *NODE PRINT,NSET=ALL,FREQ=10 U, TU, RTU, *NODE PRINT,NSET=ALL,FREQ=10,GLOBAL=YES U, TU, RTU, *NODE FILE,NSET=ALL U, TU, RTU *ENDSTEP *STEP *** STEP 5: UNCORRELATED WITH DIFFERENT LOAD CASE NUMBER *** *RANDOM RESPONSE 1,25,10,5,1 *modal damping, modal=direct 1,2,0.01 *select eigenmodes, generate 1, 2 *CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=UNCORRELATED 2000,1.,1. *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2000,DOF=1 *BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2000,DOF=6 ** *EL PRINT,FREQ=10 S, SF, *EL FILE,ELSET=ALL S, SF, *NODE PRINT,NSET=ALL,FREQ=10 U, TU, RTU, *NODE PRINT,NSET=ALL,FREQ=10,GLOBAL=YES U, TU, RTU, *NODE FILE,NSET=ALL U, TU, RTU *ENDSTEP