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Materials for Aircraft Structures

N.A. de Bruyne (Aero Research Limited)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 May 1950

Abstract

In this article the author discusses the suitability of existing materials for aircraft structures and shows that a hypothetical material derived by expanding an aluminium alloy would greatly simplify the structure of fuselages

Citation

de Bruyne, N.A. (1950), "Materials for Aircraft Structures", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 5, pp. 146-152. https://doi.org/10.1108/eb031900

Publisher

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MCB UP Ltd

Copyright © 1950, MCB UP Limited