*Heading
 Import of Continuum elements
 Shell general Section
*RESTART, TIMEMARKS=NO, WRITE, NUMBER=2
*Node
 1, 0.0, 0.0, 0.0
 2, 1.0, 0.0, 0.0
 3, 1.0, 1.0, 0.0
 4, 0.0, 1.0, 0.0
 5, 0.0, 0.0, 0.1
 6, 1.0, 0.0, 0.1 
 7, 1.0, 1.0, 0.1 
 8, 0.0, 1.0, 0.1
**
11, 0.0, 3.0, 0.0
12, 1.0, 3.0, 0.0
13, 1.0, 4.0, 0.0
14, 0.0, 4.0, 0.0
15, 0.0, 3.0, 0.1
16, 1.0, 3.0, 0.1 
17, 1.0, 4.0, 0.1 
18, 0.0, 4.0, 0.1
*Element, Type=SC8R, Elset=E1
 1, 1, 2, 3, 4, 5, 6, 7, 8
*Element, Type=SC8R, Elset=E2
 2,11,12,13,14,15,16,17,18
*Shell General Section, Elset=E1, Material=Mat1
0.1 
*Shell General Section, ELset=E2, Material=Mat1
0.1
*MATERIAL, NAME=Mat1
*ELASTIC, TYPE=ENGINEERING CONSTANTS
2.0E11, 1.0E11, 1.0E11, 0.3,0.23,0.34, 7.69E10, 7.69E10
9.0E9, 
*DENSITY
7850.0, 
*BOUNDARY
1, 1, 3
5, 1, 2
4, 1, 1
4, 3, 3
8, 1, 1
11, 1, 3
15, 1, 2
14, 1, 1
14, 3, 3
18, 1, 1
*Nset, Nset=Right
2,3,6,7,12,13,16,17
*Step
*Dynamic, Explicit, IMPROVED DT METHOD=NO
, 0.1
*Boundary, Type=Velocity
Right,1,1,0.5
*Output, Field, Number Interval=2
*Node Output
U
RF
*Element Output
SF
SE
Sth
S
E
*Output,History,Variable=Preselect,Timeint=0.1
*End Step