Buckling analysis of laminated composite conical shells
โ Scribed by Liyong Tong; Tsun Kuei Wang
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 481 KB
- Volume
- 47
- Category
- Article
- ISSN
- 0266-3538
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โฆ 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.
๐ SIMILAR VOLUMES
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
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