*HEADING
 Test import capability:
 HYPERELASTIC TEST with C3D6. 
 Transfer from Standard to Explicit: 
 Results imported from: sx_s_c3d6_hyper.inp 
 Base for  file:        xs_s_c3d6_hyper.inp
*IMPORT,STEP=1,INC=10,UPDATE=NO,STATE=YES
 TWO, 
*RESTART,TIMEMARKS=NO,NUM=2,WRITE
**
*EQUATION
** Since the S11 output is Cauchy or true stress, we need to
** determine the nominal stress for post-processing.
** Nodes 3,6,7 are tied to node 2 in dof 1 so that:
** Nominal stress (dof 1) = RF1 (@ node 2) / Original area
** (w/c is 1 x 1 = 1)
2, 
FACE42,1,1, 2,1,-1
**
**
** This is a dummy step to verify the stress imported from Standard analysis
**
*ELSET, ELSET=QA_TEST_ALLELEMS
TWO,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL,
**
*STEP
*DYNAMIC,EXPLICIT
  ,0.001
*BOUNDARY
ALL, ENCASTRE
*FILE OUTPUT,TIMEMARKS=YES, NUM=1
*EL FILE
 S,
*OUTPUT, FIELD, TIMEMARKS=YES, NUMBER INTERVAL=1
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
 S,
*OUTPUT,FIELD,VARIABLE=PRESELECT
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIMEINT=0.001
*END STEP
*STEP
*DYNAMIC,EXPLICIT
  ,0.1
*BOUNDARY,TYPE=VELOCITY, OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,10.0
***OUTPUT,HISTORY,TIME INTERVAL=0.0
***NODE OUTPUT,nset=all
**U,V,A
***ELEMENT OUTPUT,elset=TWO
**S,
***ENERGY OUTPUT
**ALLKE,ALLSE,ALLWK,ALLIE,ETOTAL
*FILE OUTPUT,TIMEMARKS=YES, NUM=4
*EL FILE
*NODE FILE
 U,
 COORD,
*OUTPUT, FIELD, TIMEMARKS=YES, NUMBER INTERVAL=4
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
 U,
 COORD,
*OUTPUT,FIELD,VARIABLE=PRESELECT
*OUTPUT,HISTORY,VARIABLE=PRESELECT,TIMEINT=0.025
*END STEP