To read this content please select one of the options below:

(excl. tax) 30 days to view and download

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

76

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

Related articles