*HEADING
 : NAFEMS CREEP BENCHMARK AXISYMMETRIC--PRESSURISED CYL (CCL24R)
 -- SECONDARY CREEP
*NODE
1,100.,0,0
9,200.,0,0.
19,100.,0,25.
27,200.,0,25.
*NGEN,NSET=BOTTOM
1,9
*NGEN,NSET=TOP
19,27
*NFILL,NSET=BASE
BOTTOM,TOP,2,9
*NSET, NSET=REST, GENERATE
10,18,2
*NCOPY, CHANGE NUMBER=100, OLD SET=BOTTOM, NEW SET=BOTTOM, SHIFT, MULTIPLE=15
0,0,0
0,0,0,0,0,1,22.5
*NCOPY, CHANGE NUMBER=100, OLD SET=TOP, NEW SET=TOP, SHIFT, MULTIPLE=15
0,0,0
0,0,0,0,0,1,22.5
*NCOPY, CHANGE NUMBER=100, OLD SET=REST, NEW SET=REST, SHIFT, MULTIPLE=15
0,0,0
0,0,0,0,0,1,22.5
*NSET, NSET=ALLN
BOTTOM, TOP, REST
*ELEMENT,TYPE=CCL24R
1, 201,203,221,219,1,3,21,19,101,103,121,119,202,212,220,210,2,12,20,10,102,112,120,110
*ELGEN,ELSET=ALL1
1, 4,2,1,7,200,10
*ELEMENT, TYPE=CCL24R
71, 1,3,21,19,1401,1403,1421,1419,1501,1503,1521,1519,2,12,20,10,1402,1412,1420,1410,1502,1512,1520,1510
*ELGEN,ELSET=ALL2
71,4,2,1
*ELSET, ELSET=CREEP
ALL1,ALL2
*SOLID SECTION,ELSET=CREEP,MATERIAL=STEEL
*MATERIAL,NAME=STEEL
*ELASTIC
200.E3,0.3
*CREEP,LAW=TIME
3.125E-14,5.
*TRANSFORM, TYPE=C, NSET=ALLN
0,0,0,0,0,1
*BOUNDARY
TOP,3,3,0
BOTTOM,3,3,0
ALLN,2,2,0
*ELSET, ELSET=INT
1,11,21,31,41,51,61,71
*STEP
 PRESCRIBED TENSILE STRESS
*STATIC
.1,1.
*DLOAD
INT,P6,200.
*EL PRINT,FREQ=10
CE, 
S, 
E, 
CENER, 
*NODE PRINT,FREQ=10
U,COORD
*END STEP
*STEP,INC=40
 CREEP RELAXATION
*VISCO,CETOL=5.E-4
.01,1000.,5.E-4
*EL PRINT
E, 
S, 
CENER, 
*EL FILE
S, 
*OUTPUT,FIELD
*ELEMENT OUTPUT
S,
*NODE FILE
COORD, 
*OUTPUT,FIELD
*NODE OUTPUT
COORD,
*NODE PRINT
U,COORD
*END STEP