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RESEARCH PAPERS

Buckling of Simply Supported Oblique Plates

[+] Author and Article Information
Y. Yoshimura, K. Iwata

Aeronautical Research Institute, University of Tokyo, Komaba, Meguro-ku, Tokyo, Japan

J. Appl. Mech 30(3), 363-366 (Sep 01, 1963) (4 pages) doi:10.1115/1.3636562 History: Received May 04, 1962; Revised January 25, 1963; Online September 16, 2011

Abstract

Based on the general theory of thin plates and shells previously developed by the first author, which holds also for oblique coordinate system, the problem of buckling of simply supported parallelogram plates is treated. Numerical values of the critical stresses of buckling under compression and shear are calculated, respectively, for plates having angles between 45 and 135 deg, and for side ratios 1 and 2.

Copyright © 1963 by ASME
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