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Noise characteristics of upper surface blown configurations: SummaryA systematic experimental program was conducted to develop a data base for the noise and related flow characteristics of upper surface blown configurations. The effect of various geometric and flow parameters was investigated experimentally. The dominant noise was identified from the measured flow and noise characteristics to be generated downstream of the trailing edge. The possibilities of noise reduction techniques were explored. An upper surface blown (USB) noise prediction program was developed to calculate noise levels at any point and noise contours (footprints). Using this noise prediction program and a cruise performance data base, aircraft design studies were conducted to integrate low noise and good performance characteristics. A theory was developed for the noise from the highly sheared layer of a trailing edge wake. Theoretical results compare favorably with the measured noise of the USB model.
Document ID
19780018937
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reddy, N. N.
(Lockheed-Georgia Co. Marietta, GA, United States)
Gibson, J. S.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Acoustics
Report/Patent Number
NASA-CR-2918
LG77ER0103
Report Number: NASA-CR-2918
Report Number: LG77ER0103
Accession Number
78N26880
Funding Number(s)
CONTRACT_GRANT: NAS1-13870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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