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Foreign Research Progress: Translations issued by the N.A.C.A.

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1942

Abstract

The present report describes a device for ascertaining the bending and buckling effect in stress measurements on shell structures accessible from one side only. Beginning with a discussion of the relationship between flexural strain and certain parameters, the respective errors of the test method for great or variable skin curvature within the test range are analyzed and illustrated by specimen examples.

Citation

(1942), "Foreign Research Progress: Translations issued by the N.A.C.A.", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 10, pp. 292-292. https://doi.org/10.1108/eb030952

Publisher

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MCB UP Ltd

Copyright © 1942, MCB UP Limited