*HEADING
 Two elements (S3) input deck to test Hashin's composite damage model (Explicit)
 uniaxial tension (off-axis angle 45 degree)
*PREPRINT,ECHO=YES,HISTORY=YES
**--------------------------------------------- Part1
*PART,NAME=PART-1
  *NODE
  *ELEMENT,TYPE=S3
  *ELSET,ELSET=EA
  *SHELL SECTION,ELSET=EA,MATERIAL=GLASS_EPOXY,ORIENT=RECT
   1.,
  *NSET,NSET=fix1
  *NSET,NSET=fix2
  *NSET,NSET=fix3
  *nset, nset=move
  *ORIENTATION,NAME=RECT
*END PART
**--------------------------------------------- Assembly-1
*ASSEMBLY,NAME=ASSEMBLY-1
*INSTANCE,NAME=PART-1-1,PART=PART-1
*END INSTANCE
*END ASSEMBLY
**--------------------------------------------- End Assembly
*elset, elset=qa_test_ea
 PART-1-1.EA,
*nset, nset=qa_test_fix1
 ASSEMBLY-1.PART-1-1.fix1,
*MATERIAL,NAME=GLASS_EPOXY
*Density
 1900.0,
*ELASTIC,TYPE=LAMINA
 53.8e9,17.9e9,0.25,8.96e9,8.96e9,6.88e9
**<E11>,<E22>,<nu12>,<G12>,<G13>,<G23>
*DAMAGE INITIATION,CRITERION=HASHIN,ALPHA=1.0
 1034e6,1034e6,27.6e6,138e6,41.4e6,69e6
** <X_T>,<X_C>,<Y_T>,<Y_C>,<S_L>,<S_T>
*DAMAGE EVOLUTION, TYPE=ENERGY, SOFTENING=LINEAR
 20e6,20e6,4.0e4,1.0e6
*amplitude, name=smooth_amp, definition=smooth step
 0.0, 0.0, 0.1, 1.0
*STEP
*Dynamic, Explicit, scale factor=0.05
 ,0.1
*BOUNDARY, amplitude=smooth_amp
 ASSEMBLY-1.PART-1-1.move, 1,1, 0.001
*Boundary
 ASSEMBLY-1.PART-1-1.fix1, 1,1
 ASSEMBLY-1.PART-1-1.fix2, 2,2
 ASSEMBLY-1.PART-1-1.fix3, 3,6
*OUTPUT, FIELD
*ELEMENT OUTPUT, elset=PART-1-1.EA
 S,E,
 DAMAGEFT,
 DAMAGEMT,
 DAMAGESHR,
*NODE OUTPUT
 U,
*OUTPUT,HISTORY, freq=1
*ELEMENT OUTPUT,ELSET=qa_test_ea
 ELDMD,
 HSNFTCRT,HSNMTCRT,
 DAMAGEFT,DAMAGEMT,DAMAGESHR,
*node output, nset=qa_test_fix1
 RF1,
*Output, history, freq=1, variable=preselect
*END STEP