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High Performance Turbine Engines

Published online by Cambridge University Press:  04 July 2016

R. H. Weir*
Affiliation:
National Gas Turbine Establishment, Pyestock

Extract

“Thunder driven, they clanged ……'thwart a heaven Pldshy with flying lightnings round the spurn o’ their feet”

Francis Thompson(1859–1907)

If it implied anything in the context of high performance turbine engines, the mutilated quotation from “The Hound of Heaven” might conjure up a vision of afterburning turbojets, or turbo-ramjets, propelling second or third generation supersonic transports at very great heights. This would be a misleading picture, and it will probably emerge that the quotation has little to do with what follows, as this is largely concerned with subsonic flight—on which I believe the economic future of aviation will depend for many years.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1962

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References

1.Hooker, S. G. (1959). Future of Air-Breathing Engines in Aviation. James Clayton Lecture to the Institution of Mechanical Engineers, December 1959.Google Scholar
2.Pearson, H. (1961). Trends in Aircraft Propulsion. Journal of the Royal Aeronautical Society, June 1961.CrossRefGoogle Scholar
3.Morley, A. W. (1958). Gas Turbines for Helicopters. Journal of the Royal Aeronautical Society, September 1958.Google Scholar
4.Ainley, D. G. (1956). The High Temperature Turbojet Engine, Journal of the Royal Aeronautical Society, Sept. 1956.Google Scholar
5.Taylor, T. A. (1961). Aero-Turbine Materials. “The Aeroplane and Astronautics,” 27th January/3rd February 1961.Google Scholar
6.Lovesey, A. C. (1959). The Art of Developing Aero-Engines. Journal of the Royal Aeronautical Society, August 1959.Google Scholar
7.Eccles, E. S. (1961). A New Method of Blade Vibration Measurement in Axial Flow Compressors and Turbines. Unpublished Bristol-Siddeley Report, May 1961.Google Scholar