Materials for Aircraft Structures

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