*HEADING
 MISES CREEP, LAW=DARVEAUX, 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=DARVEAUX
 2.25e-12, 5, 2.0e-4, 2.0, 1.0e-5, 1.0e6
*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
*STATIC
 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