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Developments in aircraft jet noise technologySignificant developments in two areas of jet noise technology are described: the development of jet noise technology relative to coannular nozzles of all types, and a recent approach to the analysis of flight effects that appears to allow simulated flight effects results to be transformed to actual flight conditions with a high degree of confidence. The coannular nozzle section presents results applicable to high-bypass-ratio turbofan engines, as well as current work on inverted-profile coannular nozzles applicable to low-bypass-ratio turbofan engines suitable for use in future supersonic cruise aircraft.
Document ID
19770011164
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gutierrez, O.
(NASA Lewis Research Center Cleveland, OH, United States)
Stone, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Aircraft Safety and Operating Problems
Subject Category
Air Transportation And Safety
Accession Number
77N18108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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