Natural frequencies of a symmetrically laminated composite beam with a mass at the free end are determined. The equations of motion for the laminated beam are derived accounting for the Poisson effect, rotary inertia and transverse shear deformation. Exact solutions are presented to demonstrate the
Vibration of a vertical cantilever with and without axial freedom at clamped end
β Scribed by S. Naguleswaran
- Publisher
- Elsevier Science
- Year
- 1991
- Tongue
- English
- Weight
- 546 KB
- Volume
- 146
- Category
- Article
- ISSN
- 0022-460X
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