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.
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/eb032342Download as .RIS
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