Cylindrical reticular composite shells
โ Scribed by V. A. Bunakov; V. D. Protasov
- Publisher
- Springer US
- Year
- 1990
- Tongue
- English
- Weight
- 931 KB
- Volume
- 25
- Category
- Article
- ISSN
- 1573-8922
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๐ SIMILAR VOLUMES
Free vibrations of thick rotating cross-ply laminated composite cylindrical shells are studied based on the "rst order shear deformation shell theory (FSDT). The governing equations of "ve degrees of freedom with consideration of Coriolis accelerations and rotary inertias are established. Analytical
A formulation and numerical solution are presented for the response and eigenfrequencies of cylindrical shells undergoing general angular velocity. This may simulate the structural dynamics of various engineering applications such as composite helicopter blades and satellites. The formulation of the
System loss factors corresponding to various shell modes have been evaluated by using a complex modulus approach. The damped free vibrations of composite cylindrical shells have been analyzed by using a first order shear deformation theory, in which one assumes a uniform distribution of the transver