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
โฆ LIBER โฆ
Free vibration of rotating thick composite cylindrical shells using layerwise laminate theory
โ Scribed by M.H. Kadivar; K. Samani
- Book ID
- 108393632
- Publisher
- Elsevier Science
- Year
- 2000
- Tongue
- English
- Weight
- 226 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0093-6413
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