Titanium in Structural Design: The Properties and Suitability of Titanium for Structural Applications Compared with the more Conventional Alloys
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1963
Abstract
THIS paper is restricted to airframe design problems; its purpose being to compare the suitability of titanium alloys with other alloys used in the past—e.g. aluminium alloys and stainless steels, with limited use of magnesium and nickel alloys and non‐stainless steels.
Citation
Baillie, I.L.G. and Coombe, T.W. (1963), "Titanium in Structural Design: The Properties and Suitability of Titanium for Structural Applications Compared with the more Conventional Alloys", Aircraft Engineering and Aerospace Technology, Vol. 35 No. 8, pp. 226-241. https://doi.org/10.1108/eb033767
Publisher
:MCB UP Ltd
Copyright © 1963, MCB UP Limited