*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).
** 
**
 VERIFICATION TEST FOR SAXA23
 RANDOM RESPONSE ANALYSIS
*RESTART,WRITE,FREQUENCY=1
*NODE
   1,1.1675, 0.
  21,1.1675,100.
*NGEN
  1,21
*ELEMENT,TYPE=SAXA23,OFFSET=100
 1,1,2,3  
*ELGEN,ELSET=EALL
 1,10,2
*SHELL SECTION,MATERIAL=MAT,ELSET=EALL
 .2,          
*MATERIAL,NAME=MAT
*ELASTIC
 30.0E6,0.3
*DENSITY
0.283, 
*ELSET,ELSET=EOUT
 1,6,10
*NSET,NSET=NOUT
 21,321
*NSET, NSET=BASE
1, 
101, 
201, 
301, 
*BOUNDARY
BASE, ENCASTRE
*PSD-DEFINITION,NAME=WHITE,TYPE=BASE
1.0E+4,0.,0.
1.0E+4,0.,3000.
*STEP
***
**   STEP 1: FREQUENCY STEP
***
*FREQUENCY, eigensolver=lanczos,SIM=NO
10, , 
*NODE PRINT,FREQ=0
U, 
*EL PRINT,FREQ=0
*OUTPUT,FIELD,FREQ=0
*NODE OUTPUT
*OUTPUT,FIELD,FREQ=0
*ELEMENT OUTPUT
*ENDSTEP
*STEP
***
**   STEP 2: CORRELATED CLOADS
***
*RANDOM RESPONSE
1,25,10,5,1
*modal damping, modal=direct
1,10,0.01
*CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=CORRELATED
1,1.,1.
*BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1,DOF=1
**
*EL PRINT, F=0
S,
SF,
*OUTPUT,FIELD,FREQ=10
*ELEMENT OUTPUT,ELSET=EOUT
S,
SF,
*NODE PRINT,NSET=NOUT, FREQ=10
U,
*OUTPUT,FIELD,FREQ=10
*NODE OUTPUT,NSET=NOUT
U,
*ENDSTEP
*STEP
***
**   STEP 3: UNCORRELATED
***
*RANDOM RESPONSE
1,25,10,5,1
*modal damping, modal=direct
1,10,0.01
*CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=UNCORRELATED
2,1.,1.
*BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2,DOF=1
**
*EL PRINT, F=0
S,
SF,
*OUTPUT,FIELD,FREQ=10
*ELEMENT OUTPUT,ELSET=EOUT
S,
SF,
*NODE PRINT,NSET=NOUT, FREQ=10
U,
*OUTPUT,FIELD,FREQ=10
*NODE OUTPUT,NSET=NOUT
U,
*ENDSTEP
*STEP
***
**  STEP 4: CORRELATED WITH DIFFERENT LOAD CASE NUMBER
***
*RANDOM RESPONSE
1,25,10,5,1
*modal damping, modal=direct
1,10,0.01
*select eigenmodes, generate
1, 10
*CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=CORRELATED
1000,1.,1.
*BASE MOTION,TYPE=ACCELERATION,LOAD CASE=1000,DOF=1
**
*EL PRINT, F=0
S,
SF,
*OUTPUT,FIELD,FREQ=10
*ELEMENT OUTPUT,ELSET=EOUT
S,
SF,
*NODE PRINT,NSET=NOUT, FREQ=10
U,
*OUTPUT,FIELD,FREQ=10
*NODE OUTPUT,NSET=NOUT
U,
*ENDSTEP
*STEP
***
**   STEP 5: UNCORRELATED WITH DIFFERENT LOAD CASE NUMBER
***
*RANDOM RESPONSE
1,25,10,5,1
*modal damping, modal=direct
1,10,0.01
*select eigenmodes, generate
1, 10
*CORRELATION,PSD=WHITE,COMPLEX=YES,TYPE=UNCORRELATED
2000,1.,1.
*BASE MOTION,TYPE=ACCELERATION,LOAD CASE=2000,DOF=1
**
*EL PRINT, F=0
S,
SF,
*OUTPUT,FIELD,FREQ=10
*ELEMENT OUTPUT,ELSET=EOUT
S,
SF,
*NODE PRINT,NSET=NOUT, FREQ=10
U,
*OUTPUT,FIELD,FREQ=10
*NODE OUTPUT,NSET=NOUT
U,
*ENDSTEP