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On vibrations of thin rotating laminated composite cylindrical shells

โœ Scribed by K.Y. Lam; C.T. Loy

Publisher
Elsevier Science
Year
1994
Weight
665 KB
Volume
4
Category
Article
ISSN
0961-9526

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๐Ÿ“œ SIMILAR VOLUMES

VIBRATIONS OF THICK ROTATING LAMINATED C
VIBRATIONS OF THICK ROTATING LAMINATED COMPOSITE CYLINDRICAL SHELLS
โœ K.Y. LAM; WU QIAN ๐Ÿ“‚ Article ๐Ÿ“… 1999 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 175 KB

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

Analysis of rotating laminated cylindric
Analysis of rotating laminated cylindrical shells by different thin shell theories
โœ K.Y. Lam; C.T. Loy ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 416 KB

The natural frequencies of the forward and backward modes of thin rotating laminated cylindrical shells are determined by using four common thin shell theories, namely Donnell's, Fluยจgge's, Love's and Sanders'. The objective is to present a unified analysis, formulated with the use of tracers so tha

Vibrations of rotating thin cylindrical
Vibrations of rotating thin cylindrical panels
โœ C.T. Loy; K.Y. Lam ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 873 KB

In this paper, the vibrations of rotating thin cylindrical panels are investigated. The d@erential equations of motion, which take into account the eflects of centrtfugal, Coriolis and initial tension, are formulated using Love'sJirst approximation theory for a thin shell theory. The analysis is car