Materials for Aircraft Structures
N.A. de Bruyne
(Aero Research Limited)
68
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
:MCB UP Ltd
Copyright © 1950, MCB UP Limited