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Recent Langley helicopter acoustics contributionsThe helicopter acoustics program at NASA Langley has included technology for elements of noise control ranging from sources of noise to receivers of noise. The scope of Langley contributions for about the last decade is discussed. Specifically, the resolution of two certification noise quantification issues by subjective acoustics research, the development status of the helicopter system noise prediction program ROTONET are reviewed and the highlights from research on blade rotational, broadband, and blade vortex interaction noise sources are presented. Finally, research contributions on helicopter cabin (or interior) noise control are presented. A bibliography of publications from the Langley helicopter acoustics program for the past 10 years is included.
Document ID
19880007263
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Morgan, Homer G.
(NASA Langley Research Center Hampton, VA, United States)
Pao, S. P.
(NASA Langley Research Center Hampton, VA, United States)
Powell, C. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Publication Information
Publication: NASA, Washington, NASA(Army Rotorcraft Technology. Volume 2: Materials and Structures, Propulsion and Drive Systems, Flight Dynamics and Control, and Acoustics
Subject Category
Acoustics
Accession Number
88N16646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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