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
โฆ LIBER โฆ
Free vibration of a three-centered arc clamped at the ends
โ Scribed by M.J. Maurizi; P.M. Belles; R.E. Rossi; M.A. De Rosa
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 151 KB
- Volume
- 161
- Category
- Article
- ISSN
- 0022-460X
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## A BSTRA CT The present paper deals with an exact solution of the title problem. Modal shapes and natural frequency coefficients are determined for a significant range of the mechanical andgeometric parameters that come into play. When the parameter I/A L z (where I is cross-sectional moment of
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