*HEADING
 input deck to test import with Hashin's composite damage model from /Xpl to /Std (Standard Analysis)
 Further compressive loading followed by tensile loading (off-axis angle 45 degree)
 Elements tested - sc6r, sc8r
*Restart, Write, number interval=40, time marks=yes
**
*Assembly, name=ASSEMBLY-1
*Instance, Instance=PART-1-1, LIBRARY=xs_x_dmg_hsntencomp_cshell_45
*Import, Update=yes, State=no
*End Instance
*End Assembly
**
*elset, elset=qa_test_ea
 PART-1-1.EA,
*nset, nset=qa_test_fix1
 ASSEMBLY-1.PART-1-1.fix1,
**
**redefine material in order to specify stabilization
*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
*DAMAGE STABILIZATION
 0.0001,0.0001,0.0001,0.0001
**
*amplitude, name=linear_amp, time=total time
 0.0, 0.0, 0.05, 2.0, 0.15, -3.0, 0.2, 0.0
**-------------------------------------------
*STEP, nlgeom=yes, inc=500
*Static
0.005, 0.2, ,0.005
*BOUNDARY, op=new, amplitude=linear_amp
 ASSEMBLY-1.PART-1-1.move, 1,1, 0.005
*Boundary, op=new
 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,Ee,
 DAMAGEFT,DAMAGEFC,
 DAMAGEMT,DAMAGEMC,
 DAMAGESHR,
*NODE OUTPUT
 U,
*OUTPUT,HISTORY, time interval=1.0e-3
*ELEMENT OUTPUT,ELSET=PART-1-1.EA
 ELDMD,STATUS,
 HSNFTCRT,HSNMTCRT,HSNFCCRT,HSNMCCRT,
 DAMAGEFT,DAMAGEMT,DAMAGESHR,DAMAGEFC,DAMAGEMC
*ELEMENT OUTPUT,ELSET=qa_test_ea
 ELDMD,
 DAMAGESHR,
*node output, nset=qa_test_fix1
 RF1,
*node output, nset=ASSEMBLY-1.PART-1-1.move
 U1,
*Output, history
*Energy Output, variable=preselect
*END STEP