*HEADING
   EXPLICIT THREE LAYER COMPOSITE PLATE:  PAGANO (1969)
*NODE
1, 0.,0.,0
11,10.,0.,0.
201,0.,1.0,0.
211,10.,1.0,0.
*NGEN,NSET=LEFT
1,201,100
*NGEN,NSET=RIGHT
11,211,100
*NFILL,NSET=EDGE
LEFT,RIGHT,10,1
*ELEMENT,TYPE=S4R
1,1,2,102,101
*ELGEN,ELSET=PLATE
1,10,1,1,2,100,10,1
*SHELL GENERAL SECTION,ELSET=PLATE,COMPOSITE, POISSON=0.0
0.125,,LAMINA, 0.
0.125,,LAMINA,90.
*MATERIAL,NAME=LAMINA
*ELASTIC,TYPE=LAMINA
25.E6,1.E6,.25,0.5E6,0.5E6,0.2E6
*FAIL STRESS
30.,-12.,.5,-1.5,1.0,0.
*FAIL STRAIN
17.E-2,-7.E-2,5.E-2,-1.3E-2,11.E-2
*DENSITY
4.5E3, 
*ELSET,ELSET=FMEAS
5,
*BOUNDARY
LEFT,1,3
RIGHT,2,3
EDGE,2
EDGE,4
EDGE,6
**
*RESTART,WRITE,NUMBER INTERVAL=2,TIMEMARKS=NO
*NSET, NSET=CHECK
LEFT, RIGHT
*NSET,NSET=QA_TEST_CHECK
CHECK,
**
*STEP
*DYNAMIC, EXPLICIT
 ,10.0
**
** Distributed load for p=p0sin(pi*x/l)
**
*CLOAD, FOLLOWER
  1,3,1.30184E-02
  2,3,7.66215E-02
  3,3,0.14574    
  4,3,0.20060    
  5,3,0.23582    
  6,3,0.24795    
  7,3,0.23582    
  8,3,0.20060    
  9,3,0.14574    
 10,3,7.66215E-02
 11,3,1.30184E-02
101,3,2.60368E-02
102,3,0.15324    
103,3,0.29149    
104,3,0.40120    
105,3,0.47163    
106,3,0.49590    
107,3,0.47163    
108,3,0.40120    
109,3,0.29149    
110,3,0.15324    
111,3,2.60368E-02
201,3,1.30184E-02
202,3,7.66215E-02
203,3,0.14574    
204,3,0.20060    
205,3,0.23582    
206,3,0.24795    
207,3,0.23582    
208,3,0.20060    
209,3,0.14574    
210,3,7.66215E-02
211,3,1.30184E-02
*MONITOR,NODE=6,DOF=3
***OUTPUT,HISTORY,TIME INTERVAL=.01
***ELEMENT OUTPUT,ELSET=PLATE
**S,
**STH,
**SF,
**SE,
***NODE OUTPUT,NSET=EDGE
**U,COORD
***ENERGY OUTPUT
**ALLKE,ALLIE,ALLSE,ALLAE,ALLVD,ALLCD,ALLPD,ALLFD,ALLWK,ETOTAL,DT
*FILE OUTPUT,NUM=4,TIMEMARKS=YES
*NODE FILE, NSET=CHECK
U,
*OUTPUT, FIELD, NUMBER INTERVAL=4, TIMEMARKS=YES
*NODE OUTPUT, NSET=QA_TEST_CHECK
U,
*OUTPUT,FIELD,VARIABLE=PRESELECT
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIMEINT=2.5
*END STEP