OUTPUT (XYPLOT XTITLE= TIME (SEC) YTITLEE BASE ACCELERATION XYPLOT ACCELERATION RESPONSE /23 (T3) YTITLEE BASE DISPLACEMENT XYPLOT DISP RESPONSE /23 (T3) YT工TLE= IP CENTER I工 SPLACEMENT RESPONSE XYPLOT DISP RESPONSE /33 (T3) BEGIN BULK s PLATE MODEL DESCRIBED IN NORMAL MODES EXAMPLE INClUDE 'plate. bdf' PARAM. COUPMASS 1 PARAM, WTMASS, 0.00259 S SPECIFY STRUCTURAL DAMPING PARAM, G, 0.06 s APPLY EDGE CONSTRAINTS sPc1,200,12456,1,12,23,34,45 s PLACE BIG FOUNDATION MASS (BFM)AT BASE CMASS2,100,1000.,23,3 S RBE MASS TO REMAINING BASE POINTS RBE2,101,23,3,1,12,34,45 s APPLY LOADING TO FOUNDATION MASS TLOAD2,500,600,,0,0.0,0.004,250.,-90 DAREA,600,23,3,2.588 S SPECIFY INTEGRATION TIME STEPSOUTPUT (XYPLOT) XGRID=YES YGRID=YES XTITLE= TIME (SEC) YTITLE= BASE ACCELERATION XYPLOT ACCELERATION RESPONSE / 23 (T3) YTITLE= BASE DISPLACEMENT XYPLOT DISP RESPONSE / 23 (T3) YTITLE= TIP CENTER DISPLACEMENT RESPONSE XYPLOT DISP RESPONSE / 33 (T3) $ BEGIN BULK $ $ PLATE MODEL DESCRIBED IN NORMAL MODES EXAMPLE $ INCLUDE ’plate.bdf’ PARAM, COUPMASS, 1 PARAM, WTMASS, 0.00259 $ $ SPECIFY STRUCTURAL DAMPING $ PARAM, G, 0.06 PARAM, W3, 1571. $ $ APPLY EDGE CONSTRAINTS $ SPC1, 200, 12456, 1, 12, 23, 34, 45 $ $ PLACE BIG FOUNDATION MASS (BFM) AT BASE $ CMASS2, 100, 1000., 23, 3 $ $ RBE MASS TO REMAINING BASE POINTS $ RBE2, 101, 23, 3, 1, 12, 34, 45 $ $ APPLY LOADING TO FOUNDATION MASS $ TLOAD2, 500, 600, , 0, 0.0, 0.004, 250., -90. $ DAREA, 600, 23, 3, 2.588 $ $ SPECIFY INTEGRATION TIME STEPS $