Thermal Fatigue Test Installation for Concorde: A description of the test procedure and the principle of operation of the system
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 March 1971
Abstract
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.
Citation
Hirschberg, H.G. (1971), "Thermal Fatigue Test Installation for Concorde: A description of the test procedure and the principle of operation of the system", Aircraft Engineering and Aerospace Technology, Vol. 43 No. 3, pp. 22-29. https://doi.org/10.1108/eb034743
Publisher
:MCB UP Ltd
Copyright © 1971, MCB UP Limited