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Free vibration analysis of laminated composite cylindrical shells by DQM

โœ Scribed by C. Shu; H. Du

Publisher
Elsevier Science
Year
1997
Tongue
English
Weight
664 KB
Volume
28
Category
Article
ISSN
1359-8368

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๐Ÿ“œ SIMILAR VOLUMES

Finite element free vibration analysis o
Finite element free vibration analysis of point supported laminated composite cylindrical shells
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

Free vibration of symmetric angle-ply th
Free vibration of symmetric angle-ply thick laminated composite cylindrical shells
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

FREE VIBRATION ANALYSIS OF COMPOSITE LAM
FREE VIBRATION ANALYSIS OF COMPOSITE LAMINATED CONICAL SHELLS BY GENERALIZED DIFFERENTIAL QUADRATURE
โœ C. Shu ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 496 KB

This paper presents the first endeavour to apply the global method of generalized differential quadrature (CDQ) to the free vibration analysis of composite laminated conical shells. The GDQ method has been developed to improve the differential quadrature (DQ) technique for the computation of weighti