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Dynamic Buckling of Composite Structures Subjected to Impulse Loads Using the Lyapunov Exponent

Department of Mechanics of Composite Materials, Faculty of Mechanics, Kim Il Sung University, Pyongyang City, Democratic People’s Republic of Korea

E-mail Address: sh.u.@ryongnamsan.edu.kp

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Yong-Il So

Department of Mechanics of Composite Materials, Faculty of Mechanics, Kim Il Sung University, Pyongyang City, Democratic People’s Republic of Korea

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Wang-Myong So

Department of Mechanics of Composite Materials, Faculty of Mechanics, Kim Il Sung University, Pyongyang City, Democratic People’s Republic of Korea

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https://doi.org/10.1142/S0219455422500869Cited by:1 (Source: Crossref)

Abstract

This paper focuses on dynamic buckling of composite structures subjected to impulse loads. Using the Lyapunov exponent, the Budiansky–Hutchinson criterion is improved and its algorithm is constructed. Based on it, the nonlinear dynamic buckling loads are evaluated for typical composite structures such as a fiber-reinforced composite plate, composite laminated cylindrical shells and a laminated plate with delaminations and matrix cracks that are all subjected to impulse loads. The improved criterion of dynamic buckling is validated through comparisons with the results in the published literatures.

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