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Advanced inlet duct noise reduction conceptsA progress report is given on the implications of inlet noise reduction on aircraft direct operating costs (DOC). It considers treated inlet rings, various other inlet noise reduction concepts, and forward-speed effects. The report was limited to relatively well-established approaches to inlet noise reduction, such as acoustic liners and fixed-geometry/high-subsonic-speed inlets which are the focus of considerable current research activity. All of the concepts discussed are of a "passive" nature, i.e., no moving parts or electrical feedback systems.
Document ID
19770011163
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chestnutt, D.
(NASA Langley Research Center Hampton, VA, United States)
Feiler, C. E.
(NASA Lewis Res. Center)
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
77N18107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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