*HEADING
: NAFEMS TEST LE10: THICK PLATE - PRESSURE
COARSE MESH, C3D20R ELEMENTS
*NODE,NSET=LAY1
*NCOPY,SHIFT,OLDSET=LAY1,NEWSET=LAY2,CHANGE NUMBER=1000
*NCOPY,SHIFT,OLDSET=LAY2,NEWSET=LAY3,CHANGE NUMBER=1000
*NCOPY,SHIFT,OLDSET=LAY3,NEWSET=LAY4,CHANGE NUMBER=1000
*NCOPY,SHIFT,OLDSET=LAY4,NEWSET=LAY5,CHANGE NUMBER=1000
*NSET,NSET=AB,GEN
*NSET,NSET=DC,GEN
*NSET,NSET=BC,GEN
*NSET,NSET=MID,GEN
*ELEMENT,TYPE=C3D20R
*ELGEN,ELSET=ALLE
*MATERIAL,NAME=MATPROP
*ELASTIC
 210.0E9,0.3
*ELSET,ELSET=LOAD,GEN
*ELSET,ELSET=EOUT
*SOLID SECTION,ELSET=ALLE,MATERIAL=MATPROP
*BOUNDARY
AB,1
DC,2
BC,1,2
MID,3
*STEP,PERT
*STATIC
*DLOAD
 LOAD,P2,  1.0E6
*NODE PRINT,FREQ=0
*EL PRINT,POSITION=AVERAGED AT NODES,ELSET=EOUT
S,
*EL FILE,POSITION=AVERAGED AT NODES,ELSET=EOUT
S,
*END STEP