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Supersonic Ram‐jet Performance: A Study of the Probable Performance of Ram‐jet Engines at High Mach Numbers

J. Lukasiewicz, B.Sc., D.I.C., Dipl.Ing. (In charge, High Speed Aerodynamics Laboratory, Natioial Aeronautical Establishment, Ottawa, Canada.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1953

Abstract

Ideal and practical performance of ram‐jet units in steady flight in the stratosphere at Mach numbers from 1·5 to 4 is examined. The effects of combustion, temperature, altitude, intake and exhaust nozzle design are considered.

Citation

Lukasiewicz, J. (1953), "Supersonic Ram‐jet Performance: A Study of the Probable Performance of Ram‐jet Engines at High Mach Numbers", Aircraft Engineering and Aerospace Technology, Vol. 25 No. 10, pp. 298-306. https://doi.org/10.1108/eb032342

Publisher

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MCB UP Ltd

Copyright © 1953, MCB UP Limited