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FESA/reference/cantilever beam/cantilever beam.inp
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2026-07-29 23:32:26 +09:00

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*Heading
** Job name: Job-1 Model name: Model-1
** Generated by: Abaqus/CAE Learning Edition 2024
*Preprint, echo=NO, model=NO, history=NO, contact=NO
**
** PARTS
**
*Part, name=Part-1
*Node
1, 0., 0., 0.
2, 1., 0., 0.
3, 2., 0., 0.
4, 3., 0., 0.
5, 4., 0., 0.
6, 5., 0., 0.
7, 6., 0., 0.
8, 7., 0., 0.
9, 8., 0., 0.
10, 9., 0., 0.
11, 10., 0., 0.
*Element, type=B31
1, 1, 2
2, 2, 3
3, 3, 4
4, 4, 5
5, 5, 6
6, 6, 7
7, 7, 8
8, 8, 9
9, 9, 10
10, 10, 11
*Nset, nset=Set-1, generate
1, 11, 1
*Elset, elset=Set-1, generate
1, 10, 1
*Nset, nset=Set-2, generate
1, 11, 1
*Elset, elset=Set-2, generate
1, 10, 1
** Section: Section-1 Profile: Profile-1
*Beam General Section, elset=Set-1, material=Material-1, section=GENERAL
1., 0.0833333, 0., 0.0833333, 0.140833
0.,1.,0.
*End Part
**
**
** ASSEMBLY
**
*Assembly, name=Assembly
**
*Instance, name=Part-1-1, part=Part-1
*End Instance
**
*Nset, nset=Set-1, instance=Part-1-1
11,
*Nset, nset=Set-2, instance=Part-1-1
1,
*End Assembly
**
** MATERIALS
**
*Material, name=Material-1
*Elastic
2.1e+11, 0.3
** ----------------------------------------------------------------
**
** STEP: Step-1
**
*Step, name=Step-1, nlgeom=NO
*Static
1., 1., 1e-05, 1.
**
** BOUNDARY CONDITIONS
**
** Name: BC-1 Type: Displacement/Rotation
*Boundary
Set-2, 1, 1
Set-2, 2, 2
Set-2, 3, 3
Set-2, 4, 4
Set-2, 5, 5
Set-2, 6, 6
**
** LOADS
**
** Name: Load-1 Type: Concentrated force
*Cload
Set-1, 3, -10000.
**
** OUTPUT REQUESTS
**
*Restart, write, frequency=0
**
** FIELD OUTPUT: F-Output-1
**
*Output, field, variable=PRESELECT
**
** HISTORY OUTPUT: H-Output-1
**
*Output, history, variable=PRESELECT
*End Step