*HEADING
 ABAQUS/Explicit benchmark problem.
 The problem simulates the penatration of a thin plate
 by a projectile. Similar to pp_velo_study but with low
 speed impact to allow completion of analysis without
 element failure. This is to simulate a balanced
 master-slave approach with the master surface at r=0.
 UNITS [kg, N, m, s]
**
*NODE, NSET=NALL
1,0.,0.
301,50.E-3,0
6,0.,1.3E-3
306,50.E-3,1.3E-3
*NGEN, NSET=CENTER
1,6,1
*NGEN, NSET=EDGE
301,306,1
*NFILL, NSET=NALL, BIAS=0.95
CENTER,EDGE,50,6
*NSET,NSET=PLATE
NALL,
**
*ELEMENT, ELSET=PLATE, TYPE=CAX4R
1,1,7,8,2
*ELGEN,ELSET=PLATE
1,50,6,1,5,1,50
**
*SOLID SECTION, ELSET=PLATE, MATERIAL=M2024T4A1
**
*MATERIAL, NAME=M2024T4A1
*ELASTIC
71.9E9,0.34
*PLASTIC
306.031E6, 0.0
367.350E6, 0.019
389.394E6, 0.039
407.510E6, 0.058
423.825E6, 0.076
439.095E6, 0.095
453.686E6, 0.113
467.801E6, 0.131
481.570E6, 0.148
495.076E6, 0.165
*DENSITY
2767.99,
**
*NODE, NSET=RREF
99999,0., -68.5E-3
*NODE, NSET=MISSILE
1000,-1.E-4, -5.E-3
1100,10.E-3, -32.47E-3
1200,10.E-3, -68.5E-3
*NGEN,NSET=MISSILE
1000,1100,1
1100,1200,1
*NSET, NSET=NALL
RREF,MISSILE
*ELEMENT, TYPE=RAX2,ELSET=MISSILE
1000,1000,1001
*ELGEN,ELSET=MISSILE
1000,200,1
*ELEMENT, TYPE=MASS, ELSET=EMASS
99999,99999
*MASS, ELSET=EMASS
0.11, 
*INITIAL CONDITION, TYPE=VELOCITY
99999,2,250.0
*BOUNDARY
EDGE,1,2
99999,1,1
99999,4,6
**
*SURFACE,TYPE=ELEMENT, NAME=PROJECTILE
MISSILE,SPOS
*SURFACE,TYPE=ELEMENT, NAME=PLATE
PLATE,
*RIGID BODY,REFNODE=99999, ELSET=MISSILE
*STEP
*DYNAMIC, EXPLICIT
,1.5E-4
**
*ADAPTIVE MESH, ELSET=PLATE, CONTROLS=TEST
*ADAPTIVE MESH CONTROLS,NAME=TEST,CURVATURE REFINEMENT=0.0
**
*CONTACT PAIR,MECHANICAL=PENALTY,WEIGHT=0.5
PROJECTILE,PLATE
**
*NSET,NSET=QA_TESTN
RREF,
*OUTPUT, FIELD, NUM=4
*NODE OUTPUT, NSET=QA_TESTN
U,
**
*OUTPUT, FIELD, OP=NEW
*NODE OUTPUT, NSET=NALL
U,
*ELEMENT OUTPUT, ELSET=PLATE
S, E
*OUTPUT, HISTORY
*NODE OUTPUT, NSET=RREF
V,
*ENERGY OUTPUT, ELSET=PLATE, VARIABLE=ALL
*ENERGY OUTPUT, ELSET=EMASS, VARIABLE=ALL
*END STEP