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Stress Analysis of Triangular Cantilever Plates: A Theoretical Investigation using the Inextensional Theory for Thin Plates

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1955

Abstract

The stress distribution in triangular cantilever plates under a uniform normal load and under a tip load is investigated theoretically. Numerical solutions are presented for plates with angles of sweep from 0 deg. to 60 deg. and with tip angles of 30 deg., 45 deg., 60 deg., 75 deg. and 90 deg.

Citation

Mansfield, E.H. and Kleeman, P.W. (1955), "Stress Analysis of Triangular Cantilever Plates: A Theoretical Investigation using the Inextensional Theory for Thin Plates", Aircraft Engineering and Aerospace Technology, Vol. 27 No. 9, pp. 287-291. https://doi.org/10.1108/eb032599

Publisher

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MCB UP Ltd

Copyright © 1955, MCB UP Limited