KOKO\Mimi
62 lines
1.6 KiB
Plaintext
62 lines
1.6 KiB
Plaintext
*Heading
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** FESA projection of the Abaqus 2024 cantilever reference model.
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** Geometry, material, section, boundary conditions, and load are unchanged.
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** SCF is set to zero because FESA does not use Abaqus slenderness compensation.
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*Preprint, echo=NO, model=NO, history=NO, contact=NO
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*Part, name=PART-1_1
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*Node
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1, 0., 0., 0.
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2, 1., 0., 0.
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3, 2., 0., 0.
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4, 3., 0., 0.
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5, 4., 0., 0.
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6, 5., 0., 0.
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7, 6., 0., 0.
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8, 7., 0., 0.
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9, 8., 0., 0.
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10, 9., 0., 0.
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11, 10., 0., 0.
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*Element, type=B31
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1, 1, 2
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2, 2, 3
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3, 3, 4
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4, 4, 5
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5, 5, 6
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6, 6, 7
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7, 7, 8
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8, 8, 9
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9, 9, 10
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10, 10, 11
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*Elset, elset=Set-1, generate
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1, 10, 1
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*Beam General Section, elset=Set-1, material=Material-1, section=GENERAL
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1., 0.0833333, 0., 0.0833333, 0.140833
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0.,1.,0.
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*Transverse Shear Stiffness
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6.73077e+10, 6.73077e+10, 0.
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*End Part
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*Assembly, name=Assembly
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*Instance, name=PART-1_1-1, part=PART-1_1
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*End Instance
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*Nset, nset=Set-3, instance=PART-1_1-1
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1,
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*Nset, nset=Set-4, instance=PART-1_1-1
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11,
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*End Assembly
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*Material, name=Material-1
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*Elastic
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2.1e+11, 0.3
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*Boundary
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Set-3, 1, 1
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Set-3, 2, 2
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Set-3, 3, 3
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Set-3, 4, 4
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Set-3, 5, 5
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Set-3, 6, 6
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*Step, name=Step-1, nlgeom=NO
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*Static
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1., 1., 1e-05, 1.
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*Cload
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Set-4, 3, -1e+06
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*End Step
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