*HEADING
 THREE LAYER COMPOSITE PLATE:  PAGANO (1969) [SC8R]
*NODE
    1,   0., 0.,  -1.25
   11,  10., 0.,  -1.25
  101,   0., 1.0, -1.25
  111,  10., 1.0, -1.25
 1001,   0., 0.,  +1.25
 1011,  10., 0.,  +1.25
 1101,   0., 1.0, +1.25
 1111,  10., 1.0, +1.25
*NGEN,NSET=EDGE
    1,11
  101,111
 1001,1011
 1101,1111
*NSET,NSET=LEFT
    1,101
 1001,1101
*NSET,NSET=RIGHT
   11,111
 1011,1111
*ELEMENT,TYPE=SC8R
 1,1,2,102,101,1001,1002,1102,1101
*ELGEN,ELSET=PLATE
 1,10,1,1
*SHELL GENERAL SECTION,ELSET=PLATE,COMPOSITE,THICKNESS MODULUS=1.E6,POISSON=0.0
 0.83333,5,LAMINA,0
 0.83333,5,LAMINA,90
 0.83333,5,LAMINA,0
*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
*ELSET,ELSET=FMEAS
 5,
*EQUATION
 2,
 1001, 1, 1.0, 1, 1, 1.0
 2,
 1101, 1, 1.0, 101, 1, 1.0
 2,
 1001, 3, 1.0, 1, 3, 1.0
 2,
 1101, 3, 1.0, 101, 3, 1.0
 2,
 1011, 3, 1.0, 11, 3, 1.0
 2,
 1111, 3, 1.0, 111, 3, 1.0
*BOUNDARY
 LEFT,2,2
 RIGHT,2,2
 EDGE,2
*STEP,PERTURBATION
*STATIC
 1.0, 
*DLOAD
 PLATE,P2NU
*EL PRINT,POSITION=AVERAGED AT NODES
 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15
 S, 
 TSHR, 
*EL PRINT
 SF, 
 SE, 
*EL FILE
 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15
 S, 
 TSHR, 
 CFAILURE,
*EL FILE
 SF,SE
*NODE FILE
 U, 
*NODE PRINT
 U, 
*EL PRINT,ELSET=FMEAS,POSITION=AVERAGED AT NODES
 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15
 CFAILURE,
*END STEP