*HEADING
 A one element (CPS4R) input deck to test composite damage model
 RIKS analysis test
*PREPRINT,ECHO=YES,HISTORY=YES
**--------------------------------------------- Part1
*PART,NAME=PART-1
  *NODE
   1,  0.0, 0.0
   2,  1.0, 0.0
   3,  1.0, 1.0
   4,  0.0, 1.0
  *ELEMENT,TYPE=CPS4R
   1,1,2,3,4
  *ELSET,ELSET=EA
   1,
  *SOLID SECTION,ELSET=EA,MATERIAL=GLASS_EPOXY,ORIENT=RECT
   1.,
  *NSET,NSET=Left
   1,4
  *NSET,NSET=bot
   1,2
  *nset, nset=right
   2, 3
  *ORIENTATION,NAME=RECT
   1.0, 0.0, 0.0, 0.0, 1.0, 0.0
   3,0.0
*END PART
**--------------------------------------------- Assembly-1
*ASSEMBLY,NAME=ASSEMBLY-1
*INSTANCE,NAME=PART-1-1,PART=PART-1
*END INSTANCE
*END ASSEMBLY
**--------------------------------------------- End Assembly
*MATERIAL,NAME=GLASS_EPOXY
*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=0.0
 1034e6,1034e6,27.6e6,138e6,41.4e6,50e6
** <X_T>,<X_C>,<Y_T>,<Y_C>,<S_L>,<S_T>
*DAMAGE EVOLUTION, TYPE=ENERGY, SOFTENING=LINEAR
 10e6,10e6,5e6,5e6
*DAMAGE STABILIZATION
  0.0001, 0.0001, 0.0001, 0.0001
*BOUNDARY
 ASSEMBLY-1.PART-1-1.left,1,1
 ASSEMBLY-1.PART-1-1.bot, 2,2
*STEP,INC=200, NLGEOM
*STATIC, RIKS
 0.01,1.0,,5.0,,PART-1-1.2,1,0.05
*DLOAD
 ASSEMBLY-1.PART-1-1.EA,P2,-10e6
*ENERGY PRINT
*NODE PRINT
 U,
*OUTPUT,FIELD
*ELEMENT OUTPUT
 DMICRT
 S,
 E,
 DAMAGEFT,
 DAMAGEFC,
 DAMAGEMT,
 DAMAGEMC,
 DAMAGESHR,
 STATUS,
*NODE OUTPUT
 U,
*OUTPUT,HISTORY
*ELEMENT OUTPUT,ELSET=PART-1-1.EA
 HSNFTCRT,
 HSNFCCRT,
 HSNMTCRT,
 HSNMCCRT,
 S,
 E,
 DAMAGEFT,
 DAMAGEFC,
 DAMAGEMT,
 DAMAGEMC,
 DAMAGESHR,
 STATUS,
*NODE OUTPUT,NSET=PART-1-1.right
 RF, U
*EL PRINT
 HSNFTCRT
*END STEP