*HEADING
 VERIFICATION TEST FOR SAXA22
 TRANSIENT DYNAMIC AND MODAL DYNAMIC ANALYSIS
*RESTART,WRITE,FREQUENCY=1
*NODE
   1,1.1675, 0.
  21,1.1675,100.
*NGEN
  1,21
*ELEMENT,TYPE=SAXA22,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
0.730E-03, 
*DAMPING, ALPHA=0.0, BETA=0.001
*ELSET,ELSET=EOUT
 1,6,10
*NSET,NSET=NOUT
 21,221
*BOUNDARY
   1,1,6
 101,1,6
 201,1,6
*AMPLITUDE, NAME=WAVE
0.0, 0.0, 0.01, 0.58777, 0.02, 0.95104, 0.03, 0.95107
0.04, 0.58784, 0.05, 9.265E-05, 0.06, -0.58769, 0.07, -0.95104
0.08, -0.95107, 0.09, 0.58792, 0.1, -1.85E-04
**
**
*STEP
*FREQUENCY, eigensolver=lanczos
20, , , 
*MODAL FILE
*EL PRINT, F=0
*NODE PRINT, F=0
*OUTPUT,FIELD,FREQ=0
*OUTPUT,HIST,FREQ=0
*END STEP
**
**
*STEP
*MODAL DYNAMIC
0.01, 0.1
*MODAL DAMPING, MODAL=DIRECT
1, 20, 0.02
*SELECT EIGENMODES, GENERATE
1,20,1
*CLOAD, AMPLITUDE=WAVE
 21,1, 5000.0
221,1,-5000.0
*EL PRINT, F=0
*NODE PRINT, F=0
*MODAL PRINT, F=0
*OUTPUT,HISTORY,FREQ=10
*NODE OUTPUT,NSET=NOUT
U,V,A
*NODE FILE, FREQ=10, NSET=NOUT
U,V,A
*END STEP
**
**
*STEP
*STEADY STATE DYNAMICS
8.0, 100.0, 5
*MODAL DAMPING, MODAL=DIRECT
1, 20, 0.02
*SELECT EIGENMODES, GENERATE
1,20,1
*CLOAD
 21,1, 5000.0
221,1,-5000.0
*EL PRINT, F=0
*NODE PRINT, F=0
*OUTPUT,HISTORY,FREQ=5
*NODE OUTPUT,NSET=NOUT
U,V,A
*NODE FILE, FREQ=5, NSET=NOUT
U,V,A
*END STEP
**
**
*STEP
*STEADY STATE DYNAMICS, DIRECT
8.0, 100.0, 5
*CLOAD
 21,1, 5000.0
221,1,-5000.0
*EL PRINT, F=0
*NODE PRINT, F=0
*OUTPUT,HISTORY,FREQ=5
*NODE OUTPUT,NSET=NOUT
U,V,A
*NODE FILE, FREQ=5, NSET=NOUT
U,V,A
*END STEP
**
**
*STEP
*DYNAMIC
0.01, 0.1
*CLOAD, AMPLITUDE=WAVE
 21,1, 5000.0
221,1,-5000.0
*NODE PRINT, FREQ=0
*EL PRINT, FREQ=0
*OUTPUT,HISTORY,FREQ=5
*NODE OUTPUT,NSET=NOUT
U,V,A
*NODE FILE, FREQ=5, NSET=NOUT
U,V,A
*END STEP