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A review of the theory of trailing edge noiseLiterature on the theory of the generation of sound by the interaction of low Mach number turbulent flow with the edge of a semi-infinite rigid plate is critically reviewed. Three different approaches to the subject are identified, consisting of theories based on (1) Lighthill's acoustic analogy; (2) the solution of special, linearized hydroacoustic problems; and (3) ad hoc aerodynamic source models. When appropriately interpreted, all relevant theories produce essentially identical predictions in the limit of very small Mach numbers. None of the theories discusses the implications of the Kutta condition, however, nor of the effect of forward flight and source motion relative to the trailing edge. An outline of a redevelopment of the theory is included to give a unified view of the problem, exhibit the significance of the various approximations, and incorporate the effect of mean motion and of the Kutta condition.
Document ID
19780018938
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Howe, M. S.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Acoustics
Report/Patent Number
BBN-3679
NASA-CR-3021
Report Number: BBN-3679
Report Number: NASA-CR-3021
Accession Number
78N26881
Funding Number(s)
CONTRACT_GRANT: NAS1-14611
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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