*HEADING
Submodel: Cantilevered plate [S3R]
Driven from the 3rd step of the global models:
shellsub_g_s3r_xpl.inp  or 
shellsub_g_s3rs_xpl.inp
GAUSS INTEGRATION WITH 6 SECTION POINTS
*PREPRINT,ECHO=YES,HISTORY=NO,MODEL=NO
*NODE
1,
5,0.,3.
31,10.,
35,10.,3.
*NGEN,NSET=NL
1,5,1
*NGEN,NSET=NR
31,35,1
*NFILL,NSET=NALL
NL,NR,6,5
*NSET,NSET=QA_TEST
NR,
*ELEMENT,TYPE=S3R,ELSET=EALL
1,1,6,7
13,1,7,2
25,3,8,4
37,4,8,9
*ELGEN,ELSET=EALL
1,2,1,1,6,5,2
13,2,1,1,6,5,2
25,2,1,1,6,5,2
37,2,1,1,6,5,2
*ELSET,ELSET=E1
1,2,13,14,25,26,37,38,
*SHELL SECTION,ELSET=EALL,MATERIAL=MAT1, SECTION=GAUSS
0.001, 6
*MATERIAL,NAME=MAT1
*ELASTIC
1.E6,0.3
*DENSITY
10., 
*BOUNDARY
NL,1,6
**********************
*AMPLITUDE,NAME=RAMP_UP,DEFINITION=SMOOTH STEP
0,0,1,1
*AMPLITUDE,NAME=RAMP_DOWN,DEFINITION=SMOOTH STEP
0,1,1,0
*STEP
*DYNAMIC,EXPLICIT
,1.0
*DLOAD,AMP=RAMP_UP
EALL,BX,1000.
*FILE OUTPUT,NUM=10
*NODE FILE
U,
***********
*OUTPUT, FIELD, NUMBER INTERVAL=1
*NODE OUTPUT,NSET=QA_TEST
U
************
*OUTPUT, FIELD, NUMBER INTERVAL=4
*NODE OUTPUT
U
*ELEMENT OUTPUT
S,LE
*OUTPUT, HISTORY, TIME INTERVAL=0.02
*NODE OUTPUT,NSET=NALL
U,V
*ENERGY OUTPUT,VAR=PRESELECT
*END STEP
***********
*STEP
*DYNAMIC,EXPLICIT
,1.0
*DLOAD,AMP=RAMP_DOWN
EALL,BX,1000.
*END STEP
***********
*STEP
*DYNAMIC,EXPLICIT
,1.0
*DLOAD,AMP=RAMP_UP
EALL,P,1.e-2
*END STEP