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A study of scattering, production, and stimulated emission of sound by vortex flowsThe basic theory of aeroacoustics of homentropic fluid media is applied to the problems of sound scattering, production, and stimulated emission. A general theory of scattering from low speed three-dimensional vortex flows is presented. Specific results are given for the horseshoe vortex and vortex ring. The noise of an elementary corotating vortex pair in various flows is calculated. It is shown that a potential flow and shear flow can substantially increase the basic pair noise. Small reverse shears can annihilate vortex pairs and eliminate the pair noise mechanism. The pair results are used to explain qualitatively the operation of noise suppression devices. The stimulated emission of a single vortex pair and four and six vortex arrays is demonstrated. The results for six vortices illustrate how external pure tones can amplify the broadband noise of a jet in agreement with recent experimental evidence.
Document ID
19790015585
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yates, J. E.
(Aeronautical Research Associates of Princeton, Inc. Princeton, NJ, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1979
Subject Category
Acoustics
Report/Patent Number
NASA-CR-3139
ARAP-363
Accession Number
79N23756
Funding Number(s)
CONTRACT_GRANT: NAS1-15033
PROJECT: RTOP 505-06-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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