*HEADING
STEEL CANTILEVER BEAM SUBJECTED TO PRESCRIBED RANDOM EXCITATION
(BASE MOTION AS TYPE ACCELERATION)
Test for *transform for nodal psd variables         
*NODE,NSET=ENDS
 1,0,0
11,1,0
*NGEN,nset=nall
 1,11
*ELEMENT,TYPE=B23,ELSET=ONE
 1,1,2
*ELGEN,ELSET=EALL
 1,10
*BEAM GENERAL SECTION,SECTION=GENERAL,DENSITY=8000,ELSET=EALL
 1E-2,8.33E-6,0,8.33E-6,16.66E-6
 0,0,-1
 2.1E11,0.807E11
*NSET,NSET=SUPP
 1, 
*NSET,NSET=TIP
 11, 
*transform,nset=nall
1,1,0,-1,1,0
*PSD-DEFINITION,NAME=BASE,TYPE=BASE,G=9.81
   0.00001,0.,1.
   0.00001,0.,19.
   0.02,0.,20.
   0.053,0.,52.
   0.053,0.,900.
   0.0022,0.,2000.
   0.00001,0.0,2001.
*NSET,NSET=ALL,GENERATE
1,11                   
*BOUNDARY
 SUPP,ENCASTRE
*RESTART,WRITE,FREQUENCY=999
*********************************************
*STEP
*FREQUENCY, eigensolver=lanczos
 10, ,
*MODAL FILE 
*EL PRINT, SUMMARY=NO, ELSET=ONE, MODE=1, LAST MODE=3
*NODE PRINT, SUMMARY=NO, MODE=1, LAST MODE=3
U,RF
*output, field, mode list
1,2,3
*node output
u,
*END STEP
**********************************************
*STEP
*RANDOM RESPONSE
20,1E4,20,,1
*modal damping, structural
 1,10,0.1
*BASE MOTION,DOF=2,LOAD CASE=1
*CORRELATION,PSD=BASE,TYPE=UNCORRELATED
1,1.
*NODE PRINT,FREQUENCY=20
 U1 ,  V1, A1, TU1,TUR3,
 RU1,RUR3
*NODE PRINT,FREQUENCY=20,global=yes
 U1 ,  V1, A1, TU1,TUR3,
 RU1,RUR3
*EL PRINT,FREQUENCY=20
SF,
*MODAL PRINT,FREQUENCY=20
GU,
*EL FILE,FREQUENCY=20,ELSET=ONE
SF,
*MODAL FILE,FREQUENCY=20
GU,
*NODE FILE,FREQUENCY=1
U,
*NODE FILE,FREQUENCY=20,NSET=SUPP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV,RRF
*NODE FILE,FREQUENCY=20,NSET=TIP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV 
*OUTPUT,FIELD,FREQUENCY=20
*ELEMENT OUTPUT,ELSET=ONE
SF,
*NODE OUTPUT,NSET=SUPP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV,RRF
*NODE OUTPUT,NSET=TIP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV
*OUTPUT,HISTORY,FREQUENCY=1
*ELEMENT OUTPUT,ELSET=ONE
SF,
*NODE OUTPUT,NSET=SUPP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV,RRF
*NODE OUTPUT,NSET=TIP
U,V,A,TU,TV,TA
RU,RV,RA,RTU,RTV 
*END STEP