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Volume 35, Issue 8
1 August 1963
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 35, Issue 8
Review Article| August 01 1963

Titanium in Structural Design: The Properties and Suitability of Titanium for Structural Applications Compared with the more Conventional Alloys

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Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1963
Aircraft Engineering (1963) 35 (8): 226–241.
https://doi.org/10.1108/eb033767

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.

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© MCB UP Limited
1963
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