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Notes on Air Breathing Engines for Supersonic Flight*

Published online by Cambridge University Press:  04 July 2016

A. W. Morley
A. W. Morley*
Affiliation:
D. Napier and Son Ltd., London
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Extract

Aircraft operate within a domain of altitude and Mach number, the limitations to which are prescribed by the present state of technical knowledge. With the perfection of the aircraft gas turbine we have witnessed the boundaries of flight recede beyond the sonic barrier and are now approaching the stage where the vastly improved propulsiorl technique will permit cruising supersonic flight. Several excellent papers referring to this subject have been given.

Type
Research Article
Information
The Aeronautical Journal , Volume 63 , Issue 577 , January 1959 , pp. 23 - 34
Copyright
Copyright © Royal Aeronautical Society 1959

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References

1.Moult, E. S. (1955). Power Plants for Supersonic FlightFifth International Aeronautical Conference, Los Angeles 1955. Institute of the Aeronautical Sciences, 1956.Google Scholar
2.Creasey, R. F. (1956). Problems of High Speed Flighl Shell Aviation News, July, August, September, 1956Google Scholar
3.Nicholson, L. F. (1957). Engine-Airframe Integration Journal of the Royal Aeronautical Society, November 1957Google Scholar
4.Leduc, Rene (1956). Early Work and Latest Realisation with Ram-Jet Engines. American Rocket Society Report 297-56, June 1956.Google Scholar
5.Samaras, D. G. (1953). Flight Regions of Supersonii Aircraft Driven by Airbreathing Propulsive Systems W.A.D.C. Technical Report, April 1953.Google Scholar
6. Contra Rotating Supersonic Compressor Engine Patent No 773149. Filed 27th April 1954. D. Napier & Son Ltd. Ejector Turbine Engine Patent Application No. 26922/56 D. Napier & Son Ltd.Google Scholar
7.Palmer, J. R. (1956). Some Aspects of Turbo-jet Perfor mance Calculation at High Flight Mach Numbers. Aircraft Engineering, November 1956.Google Scholar
8.Kremzrer, E. J. (1954). Evaluation of Effects of Drag anc Inlet Pressure Recovery on Propulsion-System Performance. N.A.C.A. T.N. 3261, August 1954.Google Scholar
9.Ashwood, P. F. (1956). A Review of the Performance of Exhaust Systems for Gas-Turbine Aero-Engines, Institution of Mechanical Engineers, 2nd November 1956.Google Scholar
10.Summerfield, Foster and Swan, (1954). Flow Separation in Supersonic Nozzles. Jet Propulsion, Vol. 24, No. 5, p. 319. September-October 1954.Google Scholar