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Stress Analysis with Brittle Lacquer: A Method for the Experimental Evaluation of Loads Developed in Components of Complex Shape

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 September 1950

Abstract

1.0 WHEN an engineer sets out to calculate the shape and dimensions of parts of machinery he becomes rapidly aware of his ignorance. Mechanical parts have such singular shapes and dimensions and are supported under such conditions that no practical method of calculation will satisfy them.

Citation

Salmon, B. (1950), "Stress Analysis with Brittle Lacquer: A Method for the Experimental Evaluation of Loads Developed in Components of Complex Shape", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 9, pp. 256-263. https://doi.org/10.1108/eb031942

Publisher

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MCB UP Ltd

Copyright © 1950, MCB UP Limited