Reduced Input
*Node and *Element Cards are removed.
*KEYWORD
*TITLE
Deformation of a Cylinder
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$ PROGRAM CONTROL & OUTPUT SECTION
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*CONTROL_TIMESTEP
0, 0.9
*CONTROL_TERMINATION
0.005
*SET_NODE_LIST
11
388, 389
*DATABASE_HISTORY_NODE_SET
11
*DATABASE_HISTORY_SHELL
340
*DATABASE_BINARY_D3PLOT
1.000E-04
*DATABASE_ABSTAT
1.000E-06
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$ DEFINE MATERIALS, SECTIONS, PARTS
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*PART
SHELL:
2, 1, 1
*MAT_ELASTIC
1, 1.497e-4, 0.1985e8, 0.30
*SECTION_SHELL
1, 2
0.14, 0.14, 0.14, 0.14
*MAT_ELASTIC
1, 1.497e-4, 0.1985e8, 0.30
$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
*PART
control volume:
3, 2, 2
*SECTION_SHELL
2, 5
0.14, 0.14, 0.14, 0.14
*MAT_ELASTIC
2, 1.497e-4, 0.1985e8, 0.3
$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
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$ DEFINE LOADING
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*LOAD_SHELL_ELEMENT
710 1 -10000.00 0.0000000
410 1 -10000.00 0.0000000
*DEFINE_CURVE
1
0, 0
0.005, -10.0
1, -10.0
$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
*SET_PART_LIST
11
3
*AIRBAG_SIMPLE_AIRBAG_MODEL
$ sid sidtyp
11 99
$rbid!=0 i
$ n
$ cv cp t lcid mu a pe ro
1.736E+03 2.430E+03 1.200E+03 2 7.000E-01 0.000E+00 1.470E+01 3.821E-06
$ i
$ lou
$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
*DEFINE_CURVE
$ lcid
2
0.000E+00 0.000E+00
1.000E+10 0.000E+00
$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
*NODE
$
*ELEMENT_SHELL
$
*BOUNDARY_SPC_NODE
$
*END