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Noise from interaction of flow with rigid surfaces: A review of current status of prediction techniquesA brief review of some fundamental aspects of sound arising from turbulent boundary layers, noise due to flow past a single discontinuity (trailing edge), noise from airfoils operating in turbulent flow, and noise due to rigid flow discontinuities (spoilers) immersed in rigid ducts is presented. Emphasis is on dipole-like sound fields associated with turbulent flow past a trailing edge, rigid bodies in turbulence and in-duct spoilers. Representative available data are reviewed and evaluated in terms of theoretical considerations and, where possible, empirical prediction techniques are given in terms of convenient aerodynamic and geometric parameters. Limitations on current knowledge are discussed.
Document ID
19720025379
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hayden, R. E.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1972
Publication Information
Publisher: NASA
Subject Category
Aircraft
Report/Patent Number
NASA-CR-2126
BBN-2276
Report Number: NASA-CR-2126
Report Number: BBN-2276
Accession Number
72N33029
Funding Number(s)
CONTRACT_GRANT: NAS1-9559-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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