Supersonic Ram‐jet Performance: A Study of the Probable Performance of Ram‐jet Engines at High Mach Numbers
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
:MCB UP Ltd
Copyright © 1953, MCB UP Limited