*HEADING
: NAFEMS TEST NL2: AXISYMMETRIC THICK CYLINDER
CAX8R ELEMENTS
*NODE,NSET=ALLN
1, 100.,0.
2, 110.,0.
3, 120.,0.
4, 130.,0.
5, 140.,0.
6, 155.,0.
7, 170.,0.
8, 185.,0.
9, 200.,0.
11, 100.,10.
13, 120.,10.
15, 140.,10.
17, 170.,10.
19, 200.,10.
21, 100.,20.
22, 110.,20.
23, 120.,20.
24, 130.,20.
25, 140.,20.
26, 155.,20.
27, 170.,20.
28, 185.,20.
29, 200.,20.
*ELEMENT,TYPE=CAX8R
1, 1,3,23,21,2,13,22,11
*ELGEN,ELSET=ALLE
1, 4,2,1
*SOLID SECTION,ELSET=ALLE,MATERIAL=M1
*MATERIAL,NAME=M1
*ELASTIC
207.E9,0.3
*PLASTIC
207.9E6, 
*BOUNDARY
ALLN,2
** Pressure=80.
*STEP
*STATIC
*DLOAD
1,P4,80.E6
*NODE PRINT,F=0
*NODE FILE,F=0
*EL PRINT,F=20
COORD,S11,S33
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=100.
*STEP
*STATIC
*DLOAD
1,P4,100.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=120.
*STEP
*STATIC
*DLOAD
1,P4,120.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=140.
*STEP
*STATIC
*DLOAD
1,P4,140.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=160.
*STEP
*STATIC
*DLOAD
1,P4,160.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP