๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Buckling analysis of laminated composite conical shells

โœ Scribed by Liyong Tong; Tsun Kuei Wang


Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
481 KB
Volume
47
Category
Article
ISSN
0266-3538

No coin nor oath required. For personal study only.

โœฆ Synopsis


Eight first-order differential equations in terms of a particularly convenient coordinate system are obtained for linear buckling analysis of laminated conical shells, with orthotropic stretching-bending coupling, under axial compressive load. These equations are solved by using the numerical integration technique and the multisegment method. By analyzing the buckling of a series of conical shells, the effects of boundary conditions, elastic coefficients and the stretchingbending coupling, on the buckling loads and circumferential wavenumbers, are investigated.


๐Ÿ“œ SIMILAR VOLUMES


The non-linear buckling analysis of cros
โœ A.H. Sofiyev; N. Kuruoglu ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 381 KB

In this study, the non-linear buckling behavior of cross-ply laminated orthotropic truncated conical shells under axial load has been investigated. The basic relations of the cross-ply laminated orthotropic truncated conical shells are derived using the von Karman-Donnell-type of kinematic non-linea

FREE VIBRATION ANALYSIS OF COMPOSITE LAM
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