A Review of Propulsion for High Mach Number Aircraft: A survey of the types of engine that will be used in the next generation of supersonic and hypersonic aircraft

Abstract

THE problem of providing engines suitable for high Mach number aircraft is a fascinating study which at the moment has only been taken to the stage where many solutions look feasible, thus the choice of engines for the different roles for which high Mach number aircraft may be used is still fairly wide open.

Citation

Lane, R.J. (1966), "A Review of Propulsion for High Mach Number Aircraft: A survey of the types of engine that will be used in the next generation of supersonic and hypersonic aircraft", Aircraft Engineering and Aerospace Technology, Vol. 38 No. 1, pp. 11-18. https://doi.org/10.1108/eb034114