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Blown flap noise predictionTheoretical and experimental developments of flow-surface interaction noise with a particular emphasis on blown-flap noise were reviewed. Several blown-flap noise prediction methods were evaluated by comparing predicted acoustic levels, directivity, and spectra with a recently obtained data base. A prediction method was selected and a detailed step-by-step description of this method was provided to develop a computer module to calculate one-third octave band frequency spectra at any given location in the far-field for under-the-wing and upper surface blown configurations as a function of geometric and operational parameters.
Document ID
19790008477
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reddy, N. N.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Acoustics
Report/Patent Number
LG78ER0237
NASA-CR-158978
Report Number: LG78ER0237
Report Number: NASA-CR-158978
Accession Number
79N16648
Funding Number(s)
CONTRACT_GRANT: NAS1-15068
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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