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Stress Diffusion Problems

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1946

Abstract

IN this section we investigate various accurate solutions of the problem of the reinforced panel by using the stress‐function. We are then able to form an idea of the accuracy of the “stringer‐sheet” solution and of the conditions which must be satisfied in order that it may be reasonably accurate for practical purposes.

Citation

Goodey, W.J. (1946), "Stress Diffusion Problems", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 7, pp. 227-234. https://doi.org/10.1108/eb031389

Publisher

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MCB UP Ltd

Copyright © 1946, MCB UP Limited