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J.Q. Ye, "Edge Effects in Cross-Ply Laminated Hollow Cylindrical Shells", in B.H.V. Topping, (Editor), "Computational Techniques for Materials, Composites and Composite Structures", Civil-Comp Press, Edinburgh, UK, pp 359-363, 2000. doi:10.4203/ccp.67.8.6

Abstract

The edge effects of self-equilibrated loads acting on the end of cross-ply laminated hollow cylinders are investigated by using three dimensional elasticity theory. The study assumes that the periodic displacement and stresses fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigen-matrix whose eigenvalues represent the decay rates of the problem. The decay rates for either symmetric or antisymmetric cross-ply laminated cylinders are found and presented. The effects of material properties on decay rates are investigated for a typical eight-layered antisymmetric cross-ply laminated cylinder.

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Front Page Browse CCP CSETS CTR IJRT Other Authors Search Purchase Guide FAQ Contact us	Civil-Comp Proceedings ISSN 1759-3433 CCP: 67 COMPUTATIONAL TECHNIQUES FOR MATERIALS, COMPOSITES AND COMPOSITE STRUCTURES Edited by: B.H.V. Topping Paper VIII.6 Edge Effects in Cross-Ply Laminated Hollow Cylindrical Shells J.Q. Ye School of Civil Engineering, University of Leeds, Leeds, United Kingdom doi:10.4203/ccp.67.8.6 purchase the full-text of this paper Full Bibliographic Reference for this paper J.Q. Ye, "Edge Effects in Cross-Ply Laminated Hollow Cylindrical Shells", in B.H.V. Topping, (Editor), "Computational Techniques for Materials, Composites and Composite Structures", Civil-Comp Press, Edinburgh, UK, pp 359-363, 2000. doi:10.4203/ccp.67.8.6 Abstract The edge effects of self-equilibrated loads acting on the end of cross-ply laminated hollow cylinders are investigated by using three dimensional elasticity theory. The study assumes that the periodic displacement and stresses fields used decay away exponentially from the end load region. The use of a recursive and successive approximation method leads to an eigen-matrix whose eigenvalues represent the decay rates of the problem. The decay rates for either symmetric or antisymmetric cross-ply laminated cylinders are found and presented. The effects of material properties on decay rates are investigated for a typical eight-layered antisymmetric cross-ply laminated cylinder. purchase the full-text of this paper (price £20) go to the previous paper go to the next paper return to the table of contents return to the book description purchase this book (price £92 +P&P)
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