*HEADING
 input deck to test import with Hashin's composite damage model from /Std to /Xpl (Explicit Analysis)
 Further tensile loading followed by compressive loading (off-axis angle 45 degree)
 Elements tested - s4r, s4, s3r
*Restart, Write, number interval=40, time marks=yes
**
*Assembly, name=ASSEMBLY-1
*Instance, Instance=PART-1-1, LIBRARY=sx_s_dmg_hsntencomp_shell_45
*Import, Update=yes, State=yes
*End Instance
*End Assembly
**
*elset, elset=qa_test_ea
 PART-1-1.EA,
*nset, nset=qa_test_fix1
 ASSEMBLY-1.PART-1-1.fix1,
**
*amplitude, name=linear_amp, time=total time
 0.0, 0.0, 0.05, 1.0, 0.15, -2.0, 0.2, 0.0,
 0.25, 1.0, 0.35, -2.0, 0.4, 0.0
**
*STEP
*Dynamic, Explicit, scale factor=0.5
 ,0.2
*BOUNDARY, op=new, amplitude=linear_amp
 ASSEMBLY-1.PART-1-1.move, 1,1, 0.001
*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,
 DAMAGEFT,DAMAGEFC,
 DAMAGEMT,DAMAGEMC,
 DAMAGESHR,
*NODE OUTPUT
 U,
*OUTPUT,HISTORY, time interval=1.0e-3
*ELEMENT OUTPUT,ELSET=qa_test_ea
 ELDMD,
 HSNFTCRT,HSNMTCRT,HSNFCCRT,HSNMCCRT,
 DAMAGEFT,DAMAGEMT,DAMAGESHR,DAMAGEFC,DAMAGEMC
*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