*HEADING
 TWO LAYER COMPOSITE PLATE +/- 45 DEG ORIENTATION [SC6R]
*SYSTEM
*NODE, NSET=BOTTOM
*NODE, NSET=TOP
*NSET,NSET=MID,GENERATE
*NGEN,NSET=LEFT
*NGEN, NSET=RIGHT
*NFILL,NSET=ALL
 LEFT, RIGHT, 32, 50
*TRANSFORM,TYPE=R,NSET=ALL
*NSET,NSET=YPARBOT,GENERATE
*NSET,NSET=YPARTOP,GENERATE
*NSET,NSET=XPARBOT,GENERATE
*NSET,NSET=XPARTOP,GENERATE
*ELEMENT,TYPE=SC6R
*ELGEN,ELSET=PLATE
*ELSET,ELSET=PR,GENERATE
*SHELL GENERAL SECTION,ELSET=PLATE,COMPOSITE, ORIENTATION=SECORI, THICKNESS MODULUS=1.E6, POISSON=0.
 .1,3,LAMINA,-45.
 .1,3,LAMINA, 45.
*TRANSVERSE SHEAR STIFFNESS
 5.0E7,5.0E7
*MATERIAL,NAME=LAMINA
*ELASTIC,TYPE=LAMINA
 40.E6,1.E6,.25,.5E6,.5E6,.5E6
*FAIL STRESS
*ORIENTATION,NAME=SECORI,SYSTEM=RECTANGULAR
*EQUATION
 xpartop, 2, 1.0, xparbot, 2, 1.0
 ypartop, 1, 1.0, yparbot, 1, 1.0
*STEP
*STATIC
*BOUNDARY
 XPARTOP, 3, 3
 XPARBOT, 3, 3
 YPARTOP, 3, 3
 YPARBOT, 3, 3
*DLOAD
 PLATE, P2, -100.
*EL PRINT,POSITION=AVERAGED AT NODES,ELSET=PR
 SF,
*OUTPUT, FIELD
*ELEMENT OUTPUT, ELSET=PR
 SF,
 CFAILURE,
*NODE OUTPUT
 U,
*NODE PRINT,NSET=MID
 U,
*EL PRINT,ELSET=PR,POSITION=AVERAGED AT NODES
 S,MSTRS,TSAIH
*END STEP