Natural Frequencies of Cross-Ply Laminated Panels with Matrix Cracks

Abstract

The matrix cracks of cross-ply laminated panels for the solution of natural frequencies were investigated. The natural frequencies were estimated by the assumption of cracks opened on one side and closed on the other side of the cross section. The results showed the effect of tunneling matrix cracks more on the stiffness than on natural frequencies.

Department(s)

Mechanical and Aerospace Engineering

International Standard Serial Number (ISSN)

0001-1452

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2001 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.

Publication Date

01 Jan 2001

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