Effect of Lamination Constitution on Buckling of Composite Laminated Cylindrical Shells under Combined Loads
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概要
- 論文の詳細を見る
Advanced fiber-reinforced laminated composite materials have been used for structural members because of their high specific strength and stiffness. Such composite laminated structures behave differently from homogeneous orthotropic structures. In this paper, the effect of lamination constitution on the buckling strength of cross-ply and angleply laminated cylindrical shells under the simulatneous action of axial compression and external pressure is analysed by assuming the buckling patterns which exactly satisfy the Flugge-type equilibrium equations. The effects of various factors such as stacking sequence, number of layers, lamination angle, buckling mode and dimension of cylinder, on the buckling strength are analytically clarified.
- 東海大学の論文
著者
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KASUYA Hirakazu
Department of Prime Mover Engineering
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Nagai Jun
Course Of Mechanical Engineering
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KASUYA Hirakazu
Department of Mechanical Engineering, Tokai University
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