The equations for the vibration of a rotating beam, such as a helicopter blade, are exhibited. The beam is elastic (in general non-linearly so), the description is geometrically exact, the axis of rotation does not necessarily pass through the beam's clamped end (precession) and cross-sectional shea
β¦ LIBER β¦
Nonlinear vibrations and buckling of a flexible rotating beam: A prescribed torque approach
β Scribed by F.S.M. Jarrar; M.N. Hamdan
- Publisher
- Elsevier Science
- Year
- 2007
- Tongue
- English
- Weight
- 757 KB
- Volume
- 42
- Category
- Article
- ISSN
- 0094-114X
No coin nor oath required. For personal study only.
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