Hostname: page-component-848d4c4894-4hhp2 Total loading time: 0 Render date: 2024-06-04T01:55:58.794Z Has data issue: false hasContentIssue false

Propulsion

Published online by Cambridge University Press:  28 July 2016

A. V. Cleaver*
Affiliation:
Formerly de Havilland Engine Co. Ltd.

Extract

Few aeronautical engineers would disagree that the development of new propulsive systems has been the main influence responsible for the achievement of supersonic flight. This is not the same thing as claiming that sustained flight at these speeds, over fairly long ranges and with reasonable economy, would ever be possible without correspondingly large contributions from the aerodynamicist, the structural engineer, and the designers of various equipment. However, if we had been limited for all time to the piston engine/ propeller power plant almost universally employed juring the first 40 years of heavier-than-air flight, it is unlikely that we should ever have exceeded a Mach number of one.

Type
Supersonic Flight
Copyright
Copyright © Royal Aeronautical Society 1956

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Moult, E. S. (1955). Power Plants for Supersonic Flight. Proceedings of the Fifth International Aeronautical Conference, Los Angeles, 1955. Institute of the Aeronautical Sciences, 1956.Google Scholar
2. Ainley, D. G. (1956). The High Temperature Turbo-jet Engine. Journal of the Royal Aeronautical Society, September, p. 563, 1956.Google Scholar
3. Brennan, M. J. (1956). Mixed Power in Modern Aircraft. Royal Aeronautical Society Main Lecture, 1955.Google Scholar
4. Baxter, A. D. (1955). The Prospects and Problems of Rocket Propulsion for Aircraft. Journal of the Royal Aeronautical Society, May 1955.Google Scholar
5.C.I.O.S. Report 23, Item 5, File XXVIII-53, on projects of Walterwerke, Kiel.Google Scholar
6.Aeroplane, 28th October 1955.Google Scholar
7. Sänger, E. and Bredt, I. (1944). A Rocket Drive for Long Range Bombers. Deutsche Luftfahrtforschung UM 3538 in 1944, reprinted as English translation 1955 by Robert Cornog, Calif., U.S.A.Google Scholar
8.Interavia, Vol. X, No. 5 (1955).Google Scholar
9.Aero Digest, December 1953 and February 1954.Google Scholar
10. Moeckel, W. E. (1954). Use of Aerodynamic Heating to provide Thrust by Vaporization of Surface Coolants. N.A.C.A. (Unclassified) T.N. No. 3140, February 1954.Google Scholar