TECHNICAL PAPERS
Jul 1, 2005

Low-Velocity Impact Dynamic Behavior of Laminated Composite Nonprismatic Folded Plate Structures

Publication: Journal of Engineering Mechanics
Volume 131, Issue 7

Abstract

In this paper, the higher-order shear deformation theory is used to study the response of graphite/epoxy laminated composite nonprismatic folded plates subjected to impact loads. A finite-element model of the theory is also developed. The modified Hertzian contact law incorporated within the Newton–Raphson method is used to calculate the contact force between the impactor and the laminated plate. For time integration, the Newmark direct integration was adopted. Numerical results are presented to demonstrate the effects of span-to-thickness ratio, fiber angle, stacking sequence, and crank angle on the response of laminated plate subjected to impact. It is demonstrated that the results obtained from the present investigation compare well with those reported in the open literature.

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Information & Authors

Information

Published In

Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 131Issue 7July 2005
Pages: 678 - 688

History

Received: Jun 24, 2003
Accepted: Aug 11, 2004
Published online: Jul 1, 2005
Published in print: Jul 2005

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Notes

Note. Associate Editor: Arif Masud

Authors

Affiliations

Kyoung Sik Chun [email protected]
Doctoral Candidate, Dept. of Civil Engineering, The Univ. of Seoul, Seoul 130-743, Korea. E-mail: [email protected]
Samuel Kinde Kassegne [email protected]
Visiting Scientist, Dept. of Aerospace and Mechanical Engineering, Henri Samueli School of Engineering, Univ. of California, Irvine, Irvine, CA 92697-3975. E-mail: [email protected]

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