Tension buckling and postbuckling of nanocomposite laminated plates with in-plane negative Poisson’s ratio
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University , Shanghai 200240 , China
2. Department of Mechanical and Aerospace Engineering, Syracuse University , Syracuse , NY 13244 , United States of America
Abstract
Publisher
Walter de Gruyter GmbH
Link
https://www.degruyter.com/document/doi/10.1515/ntrev-2023-0173/pdf
Reference51 articles.
1. Shen H-S. Postbuckling Behavior of Plates and Shells. Singapore: World Scientific Publishing Co. Pte. Ltd; 2017.
2. Shimizu S, Yoshida S, Enomoto N. Buckling of plates with a hole under tension. Thin-Walled Struct. 1991;12:35–49.
3. Shimizu S. Tension buckling of plate having a hole. Thin-Walled Struct. 2007;45:827–33.
4. Kremer T, Schurmann H. Buckling of tension-loaded thin-walled composite plates with cut-outs. Compos Sci Technol. 2008;68:90–7.
5. Fujimoto T, Sumi S. Postbuckling behavior of centrally cracked plates under tension. JSME Int J. 1987;30:1714–23.
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