Journal
COMPOSITES PART B-ENGINEERING
Volume 51, Issue -, Pages 318-326Publisher
ELSEVIER SCI LTD
DOI: 10.1016/j.compositesb.2013.03.029
Keywords
Layered structures; Buckling; Finite deflection; Analytical modeling
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In this study, the response of a FG (functionally graded) coated truncated conical shell subjected to an axial load is investigated by means of non-linear equations governing the finite deformations of the shell. In the solution of non-linear basic equations in the finite deflection the Superposition and Galerkin methods have been used. The effects of material property of FG composite coatings and geometrical parameters on the non-linear critical axial load are discussed in detail through a parametric study. The results are verified by comparing the obtained values with those in the existing literature. (C) 2013 Elsevier Ltd. All rights reserved.
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