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Variable stream control engine concept for advanced supersonic aircraft: Features and benefitsThe Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited. Two separate flow streams, each with independent burner and nozzle systems are incorporated within the engine. By unique control of the exhaust temperatures and velocities in two coannular streams, significant reduction in jet noise is obtained.
Document ID
19770011068
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howlett, R. A.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Proc. of the SCAR Conf., Part 1
Subject Category
Aircraft Propulsion And Power
Accession Number
77N18012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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