General loading
Problem description
Model:
Length | 15.0 |
Elbow section data | = 10.0, t = 1.0 |
Centrifugal axis of rotation | (0, 0, 1) through midspan |
Gravity load vector | (0, 0, 1) |
Material:
Young's modulus | 3 × 106 |
Poisson's ratio | 0.3 |
Density | 1.0 |
Coefficient of thermal expansion | 0.0001 |
Initial conditions
Initial temperature | ALL, −10.0 |
General:
The boundary condition NODEFORM is used for load types BX, BY, BZ, GRAV, CENT, CENTRIF, and ROTA on ELBOW31 and ELBOW32 elements, preventing cross-sectional deformations.
Results and discussion
The calculated reactions are in agreement with the applied loads.
Input files
- exel1xd1.inp
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ELBOW31: BX, BY, BZ, GRAV, CENT, PI, CENTRIF, TEMPERATURE, perturbation step with LOAD CASE.
- exel1xdr.inp
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ELBOW31: ROTA.
- exelbxd1.inp
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ELBOW31B: BX, BY, BZ, GRAV, CENT, PI, CENTRIF, TEMPERATURE.
- exelbxdr.inp
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ELBOW31B: ROTA.
- exelcxd1.inp
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ELBOW31C: BX, BY, BZ, GRAV, CENT, PI, CENTRIF, TEMPERATURE.
- exelcxdr.inp
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ELBOW31C: ROTA.
- exel2xd1.inp
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ELBOW32: BX, BY, BZ, GRAV, CENT, PI, CENTRIF, TEMPERATURE.
- exel2xdr.inp
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ELBOW32: ROTA.