*HEADING
 Transfer from Standard to Explicit : Demonstrate the change 
 of material definition to include *SHEAR FAILURE in Explicit. 
 9 x 9 mesh with CPE4R is used. 
 - Standard analysis
 - loading in non-uniform biaxial tension
*NODE,NSET=ALL
 1, 1.
91, 8.
100, 8.,7.
10, 1.,7.
*NGEN,NSET=NL
1,10,1
*NGEN,NSET=NR
91,100
*NFILL,NSET=ALL
NL,NR,9,10
*NSET,NSET=FIX1,GEN
 1,91,10
*NSET,NSET=FIX2,GEN
91,100
*NSET,NSET=FIX3,GEN
10,100,10
*NSET,NSET=FIX4,GEN
1,10
*ELEMENT, TYPE=CPE4R, ELSET=EALL
 1, 1,11,12,2
*ELGEN,ELSET=EALL
1,9,1,1,9,10,10
*ELSET,ELSET=EDGE2,GEN
81,89
*SOLID SECTION,MATERIAL=RHA, ELSET=EALL
*MATERIAL,NAME=RHA
*DENSITY
 7800., 
*ELASTIC
 207.8E9, .3
*PLASTIC
 1220.E6, 0.
 2440.E6, 1.
*BOUNDARY
 FIX1, YSYMM
 FIX4, XSYMM 
*AMPLITUDE, NAME=LOADING
0., 0., 1., 3050.0E6
*RESTART,WRITE
*STEP, NLGEOM, INC=50 
*STATIC 
0.1, 1.0
*CLOAD, AMPLITUDE=LOADING 
100, 2, 0.014403292
90,  2, 0.086419753
80,  2, 0.172839506  
70,  2, 0.259259259
60,  2, 0.345679012
50,  2, 0.432098765
40,  2, 0.518518518
30,  2, 0.604938271
20,  2, 0.691358024
10,  2, 0.374485596
*CLOAD, AMPLITUDE=LOADING 
100, 1, 0.014403292
99,  1, 0.086419753
98,  1, 0.172839506  
97,  1, 0.259259259
96,  1, 0.345679012
95,  1, 0.432098765
94,  1, 0.518518518
93,  1, 0.604938271
92,  1, 0.691358024
91,  1, 0.374485596
*PRINT,FREQ=1 
*EL FILE, DIRECTIONS=YES
 S,E
*NODE FILE
 U,COORD
*EL PRINT,FREQ=1
 S,
 E,
 PEEQ,
*ENERGY PRINT, FREQ=1
 ALLKE,ALLSE,ALLWK,ALLIE,ETOTAL
*NODE PRINT,FREQ=1, NSET=FIX2 
 U,
 COORD,
 RF,
*END STEP