*HEADING
 MISES CREEP, LAW=ANAND, UNIAXIAL TENSION CREEP, C3D8
*PART,NAME=PART-1
*NODE,NSET=ALLN
1,0.,0.,0.
2,1.,0.,0.
3,1.,1.,0.
4,0.,1.,0.
5,0.,0.,10.
6,1.,0.,10.
7,1.,1.,10.
8,0.,1.,10.
*ELEMENT,TYPE=C3D8,ELSET=SPEC
1,1,2,3,4,5,6,7,8
*SOLID SECTION,ELSET=SPEC,MATERIAL=DATTIM
*END PART
*ASSEMBLY,NAME=ASSEM-1
*INSTANCE,NAME=INST-1,PART=PART-1
*END INSTANCE
*END ASSEMBLY
*Distribution Table, name=distTableElastic
 modulus, ratio
*Distribution, name=distElastic, table=distTableElastic, location=element
 , 10.e3, 0.25
 ASSEM-1.INST-1.SPEC, 20.0E6, 0.3
*MATERIAL,NAME=DATTIM
*ELASTIC
 distElastic,
*CREEP,LAW=ANAND
** S1      Q/R      A      CSI     m       A0        Shat         n
 10000.0, 5.0,   0.25E-13,  1.0,  0.5,    1.0E4,     1.0E-4,     1.0,
** ** a       S2      S3     A1       A2        A3           A4
   1 .6,   -500.0,    0.,   -600.0,   0.0,       0.0,        0.0
**  ** S1      Q/R      A      CSI     m       A0        Shat         n
**  28.6E6, 10278.43, 177016., 7.,   0.207, -90939.8E6, 52.4E6,     0.0177,
** ** a       S2      S3     A1       A2        A3           A4
** 1.6,  -0.0673E6, 0., 960.7E6, -0.956E6,  -3260581.8E6,24976815.5E6
*PHYSICAL CONSTANTS,ABSOLUTE ZERO=0.0
*BOUNDARY
 ASSEM-1.INST-1.1,PINNED
 ASSEM-1.INST-1.2,2
 ASSEM-1.INST-1.5,2
 ASSEM-1.INST-1.6,2
 ASSEM-1.INST-1.4,1
 ASSEM-1.INST-1.5,1
 ASSEM-1.INST-1.8,1
 ASSEM-1.INST-1.2,3
 ASSEM-1.INST-1.3,3
 ASSEM-1.INST-1.4,3
*INITIAL CONDITIONS,TYPE=TEMPERATURE
 ASSEM-1.INST-1.ALLN, 10.0
*STEP,AMPLITUDE=RAMP
*VISCO,CETOL=5.E-6
1.,1.
*DLOAD
 ASSEM-1.INST-1.1,P2,-20000.
*OUTPUT,FIELD,FREQ=10
*ELEMENT OUTPUT
 S,E,CE
*END STEP
*STEP,INC=100
*VISCO,CETOL=5.E-6
 0.01,100000.,1.E-3
*END STEP