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Supersonic propulsion technology
A. G. Powers, R. E. Coltrin, L. E. Stitt, Richárd Wéber, J. B. Whitlow
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Abstract
Propulsion concepts for commercial supersonic transports are discussed. It is concluded that variable cycle engines, together with advanced supersonic inlets and low noise coannular nozzles, provide good operating performance for both supersonic and subsonic flight. In addition, they are reasonably quiet during takeoff and landing and have acceptable exhaust emissions.