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Vibration Analysis of Thick Laminated Composite Cylindrical Shells

โœ Scribed by Lam, K. Y.; Ng, T. Y.; Qian, Wu

Book ID
120431063
Publisher
American Institute of Aeronautics and Astronautics
Year
2000
Tongue
English
Weight
194 KB
Volume
38
Category
Article
ISSN
0001-1452

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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

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โœ K.Y. Lam; Wu Qian ๐Ÿ“‚ Article ๐Ÿ“… 2000 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 178 KB

Analytical solutions for the vibrations of thick symmetric angle-ply laminated composite cylindrical shells are established using the firstorder shear deformation theory. The complex method is developed to deal with the partial differential governing equations of thick symmetric angle-ply laminated

Finite element free vibration analysis o
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โœ D. Chakravorty; J.N. Bandyopadhyay; P.K. Sinha ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 433 KB

A finite element analysis for the free vibration behaviour of point supported laminated composite cylindrical shells is presented. Eight-noded curved quadrilateral isoparametric elements are used. The formulation is based on the assumptions of the first order shear deformation theory for thin, shall