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Elastically Encastré Struts: A Suggestion for the Stressing of Members Subject to End Restraint

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 April 1938

Abstract

THE assumption of a pin‐jointed end condition will give optimistic results when the stress condition near the ends of a strut in a rigid‐jointed frame are of importance. The method given in this note suggests a means of determining the stress distribution in such cases.

Citation

Cook, F.G.R. and Tye, W. (1938), "Elastically Encastré Struts: A Suggestion for the Stressing of Members Subject to End Restraint", Aircraft Engineering and Aerospace Technology, Vol. 10 No. 4, pp. 103-106. https://doi.org/10.1108/eb030299

Publisher

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MCB UP Ltd

Copyright © 1938, MCB UP Limited