*HEADING
 Test import capability:
 HYPERFOAM TEST - UNIAXIAL COMPRESSION
 UNI + SS DATA - C3D10M - N=3.
 Transfer from Standard to Explicit: 
 Results imported from: sx_s_c3d10m_hfoam.inp 
 Base for  file:        xs_s_c3d10m_hfoam.inp
*IMPORT,STEP=1,INC=16,UPDATE=NO,STATE=YES
 ONE,
*RESTART,TIMEMARKS=NO,NUM=2,WRITE
**
*EQUATION
** The stress output S is Cauchy or true stress and strain output E is 
** accumulated strain. For postprocessing purposes (to compare with 
** test data), nominal stress and strain values are needed and we can
** do the following:
** Nodes 3,6,7 (NSET=FACE42) are tied to node 2 in dof 1 so that:
** Nominal stress (dof 1) = RF1 (@ node 2) / Original area (1 x 1 = 1)
** Nominal strain can be requested with the NE output identifier.
2, 
FACE42,1,1, 2,1,-1
**
**
*ELSET, ELSET=QA_TEST_ALLELEMS
ONE,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL,
**
*STEP
 This is a dummy step to verify the initial stress imported from Standard
*DYNAMIC,EXPLICIT
  ,0.0001
*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=0.0001
***OUTPUT,HISTORY,VARIABLE=PRESELECT
*END STEP
**
*STEP
*DYNAMIC,EXPLICIT
  ,0.1
*BOUNDARY,TYPE=VELOCITY, OP=NEW
FACE1,3
FACE3,2
FACE6,1
FACE4,1,1,-2.
*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