*HEADING
: NAFEMS TEST NL2: AXISYMMETRIC THICK CYLINDER
Benchmark test for CCL24R Elements
*NODE,NSET=BASE
1, 100.,0,0.
2, 110.,0,0.
3, 120.,0,0.
4, 130.,0,0.
5, 140.,0,0.
6, 155.,0,0.
7, 170.,0,0.
8, 185.,0,0.
9, 200.,0,0.
11, 100.,0,10.
13, 120.,0,10.
15, 140.,0,10.
17, 170.,0,10.
19, 200.,0,10.
21, 100.,0,20.
22, 110.,0,20.
23, 120.,0,20.
24, 130.,0,20.
25, 140.,0,20.
26, 155.,0,20.
27, 170.,0,20.
28, 185.,0,20.
29, 200.,0,20.
*NCOPY, CHANGE NUMBER=100, OLD SET=BASE, NEW SET=ALLN, SHIFT, MULTIPLE=15
0,0,0
0,0,0,0,0,1,22.5
*NSET, NSET=ALLN
ALLN, BASE
*ELEMENT,TYPE=CCL24R
1,201,203,223,221,1,3,23,21,101,103,123,121,202,213,222,211,2,13,22,11,102,113,122,111
*ELGEN,ELSET=ALL1
1, 4,2,1,7,200,10
*ELEMENT, TYPE=CCL24R
71, 1,3,23,21,1401,1403,1423,1421,1501,1503,1523,1521,2,13,22,11,1402,1413,1422,1411,1502,1513,1522,1511
*ELGEN,ELSET=ALL2
71,4,2,1
*ELSET, ELSET=ALL
ALL1,ALL2
*ELSET, ELSET=INT
1,11,21,31,41,51,61,71
*SOLID SECTION,ELSET=ALL,MATERIAL=M1
*MATERIAL,NAME=M1
*ELASTIC
207.E9,0.3
*PLASTIC
207.9E6,
*TRANSFORM, TYPE=C, NSET=ALLN
0,0,0,0,0,1
*NSET, NSET=BOUND1, GENERATE
1,9,1
21,29,1
101,109,1
121,129,1
201,209,1
221,229,1
301,309,1
321,329,1
401,409,1
421,429,1
501,509,1
521,529,1
601,609,1
621,629,1
701,709,1
721,729,1
801,809,1
821,829,1
901,909,1
921,929,1
1001,1009,1
1021,1029,1
1101,1109,1
1121,1129,1
1201,1209,1
1221,1229,1
1301,1309,1
1321,1329,1
1401,1409,1
1421,1429,1
1501,1509,1
1521,1529,1
*BOUNDARY
BOUND1,3
11,2
411,2
811,2
1211,2
** Pressure=80.
*STEP
*STATIC
*DLOAD
INT,P6,80.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
0.01,1,,0.1
*DLOAD
INT,P6,100.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=120.
*STEP
*STATIC
*DLOAD
INT,P6,120.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=140.
*STEP
*STATIC
*DLOAD
INT,P6,140.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP
** Pressure=160.
*STEP
*STATIC
*DLOAD
INT,P6,160.E6
*NODE FILE,F=0
*EL FILE,F=20
COORD,S
*ENDSTEP