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New developments in blown flap noise technologyThe noise technology relating to blown-flap systems is reviewed. There are three general sources of noise: turbomachinery, airframe, and the interaction noise of the jet blowing on the flaps. The latter noise-source area is the most critical and the main subject dicussed. Characteristics of lower surface blown and upper surface blown systems are described, including noise spectra, directivity, jet velocity characteristics, aircraft geometric variation effects, and aircraft forward speed effects. Noise reduction concepts are described, including slowing down the jet flow field by devices and engine cycle modifications, structural geometry and shielding modifications, local flow field modifications of the passive and active type, and the absorption of noise. It is concluded that, while there has been considerable progress in the past several years, low noise characteristics in blown flap aircraft must be largely built in by better application of low noise principles during the design.
Document ID
19770003071
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gibson, J. S.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-145086
Report Number: NASA-CR-145086
Meeting Information
Meeting: Congr. of ICAS
Location: Ottawa
Start Date: October 3, 1976
End Date: October 8, 1976
Accession Number
77N10013
Funding Number(s)
CONTRACT_GRANT: NAS1-13870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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