*HEADING
   TWO LAYER COMPOSITE PLATE +/- 45 DEG ORIENTATION   
*SYSTEM
   1.,2.,5. ,   2.,3.,5.
   0.,3.,6.
*NODE
1, 0.,0.,0
33,10.,0.,0.
1601,0.,10.,0.
1633,10.,10.,0.
*NSET,NSET=MID,GENERATE
801,817
*NGEN,NSET=BOT
1,33
*NGEN, NSET=TOP
1601,1633
*NFILL,NSET=ALL
BOT,TOP,32,50
*TRANSFORM,TYPE=R,NSET=ALL
1.,1.,0.,  -1.,1.,1.
*NSET,NSET=YPAR,GENERATE
1,1601,50
33,1633,50
*NSET,NSET=XPAR,GENERATE
1,33
1601,1633
*ELEMENT,TYPE=STRI65
    1,     1,     5,   205,     3,   105,   103
50001,     1,   205,   201,   103,   203,   101
*ELGEN,ELSET=PLATE
    1,     8,     4,     1,     8,   200,     8
50001,     8,     4,     1,     8,   200,     8
*ELSET,ELSET=PR
28,29,36,37
*SHELL SECTION,ELSET=PLATE,COMPOSITE
.1,3,LAMINA,LAYER1
.1,3,LAMINA,LAYER2
*TRANSVERSE SHEAR STIFFNESS
5.0E7,5.0E7
*MATERIAL,NAME=LAMINA
*ELASTIC,TYPE=LAMINA
40.E6,1.E6,.25,.5E6,.5E6,.5E6
*FAIL STRESS
60.E4,-24.E4,1.E4,-3.E4,2.0E4,0.
*ORIENTATION,NAME=LAYER1,SYSTEM=RECTANGULAR
1.,1.,0.,-1.,1.,1.
3,-45.
*ORIENTATION,NAME=LAYER2,SYSTEM=RECTANGULAR
1.,1.,0.,-1.,1.,1.
3,45.
*STEP
*STATIC
*BOUNDARY
XPAR,2,3
YPAR,1
YPAR,3
*DLOAD
PLATE,P,100.
*EL PRINT,POSITION=AVERAGED AT NODES,ELSET=PR
SF,
*EL FILE,POSITION=AVERAGED AT NODES,ELSET=PR
SF,
CFAILURE,
*NODE FILE,NSET=MID
U,
*NODE PRINT
U,
*EL PRINT,ELSET=PR,POSITION=AVERAGED AT NODES
1,2,3,4,5,6
S,MSTRS,TSAIH
*END STEP