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Volume 43, Issue 3
1 March 1971
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 43, Issue 3
Review Article| March 01 1971

Thermal Fatigue Test Installation for Concorde: A description of the test procedure and the principle of operation of the system

H.G. Hirschberg
H.G. Hirschberg
Sulzer Brothers Ltd.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1971
Aircraft Engineering (1971) 43 (3): 22–29.
https://doi.org/10.1108/eb034743

THE requirements of commercial efficiency impose a life of 12 to 15 years, coupled with a high rate of utilization, on civil aircraft. This puts very special conditions for the construction of the airframe, as well as on the testing of its reliability and safety in service.

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© MCB UP Limited
1971
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