*Heading
     Model mode I crack propagation with XFEM
** Generated by: Abaqus/CAE Version 6.9-DEV
*Preprint, echo=NO, model=yes, history=yes, contact=NO
**
*Node
*Element, type=CPE4
*Nset, nset=_PickedSet11, generate
*Elset, elset=_PickedSet11, generate
*Elset, elset=one
*enrichment,elset=_PickedSet11,interaction=lower,type=propagation crack, name=abc
** Section: Section-1
*Solid Section, elset=_PickedSet11, material=Material-1
1.0
**
*Nset, nset=_PickedSet4
*Nset, nset=_PickedSet5
*Elset, elset=_PickedSet5
*Nset, nset=_PickedSet6
*Elset, elset=_PickedSet6
**
** MATERIALS
**
*Material, name=Material-1
*Elastic
 2.1e+11, 0.3
*DAMAGE INITIATION,CRITERION=MAXPS
8.44E7
**DAMAGE EVOLUTION,TYPE=ENERGY,MIXED MODE BEHAVIOR=POWER LAW,POWER=1.0
**4.22d4,4.22d4
**DAMAGE STABILIZATION
** 1.e-5
*surface interaction,name=lower
*surface behavior
*FRACTURE CRITERION,TYPE=FATIGUE,MIXED MODE BEHAVIOR=POWER
**surface behavior, pressure-overclosure=linear
**6.42E13
**
*initial condition,type=enrichment
400,1,abc, 1.0, 0.0
400,2,abc, 1.0,-1.0
400,3,abc,-1.0,-1.0
400,4,abc,-1.0, 0.0
401,1,abc, 1.0,-1.0
401,2,abc, 1.0,-2.0
401,3,abc,-1.0,-2.0
401,4,abc,-1.0,-1.0
402,1,abc, 1.0,-2.0
402,2,abc, 1.0,-3.0
402,3,abc,-1.0,-3.0
402,4,abc,-1.0,-2.0
**
*nset,nset=disp
*equation
_PickedSet5,2,1,9999,2,-1
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
_PickedSet4, 1, 1
*amplitude,name=amp1
0,0,0.5,1,1.0,0
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step,inc=10000
*direct cyclic,fatigue
**
*controls,type=direct cyclic
,100,1E-3,100,1E-3
** BOUNDARY CONDITIONS
**
** Name: BC-2 Type: Displacement/Rotation
*Boundary,amp=amp1
9999, 2, 2, 0.00008
**_PickedSet5, 2, 2, 0.001
** Name: BC-3 Type: Displacement/Rotation
*Boundary,amp=amp1
_PickedSet6, 2, 2, -0.00008
**
**
** FIELD OUTPUT: F-Output-1
**
*Output, field,freq=50
*element output
S
*node output
U,PHILSM
*output,history,freq=50
*node output,nset=disp
rf2,u2
*element output,elset=one
S,
*End Step