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Supersonic propulsion technologyPropulsion 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.
Document ID
19800001977
Document Type
Conference Paper
Authors
Powers, A. G. (NASA Lewis Research Center Cleveland, OH, United States)
Coltrin, R. E. (NASA Lewis Research Center Cleveland, OH, United States)
Stitt, L. E. (NASA Lewis Research Center Cleveland, OH, United States)
Weber, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Whitlow, J. B., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Aeropropulsion 1979
Subject Category
AIRCRAFT PROPULSION AND POWER
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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