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Sound generated in the vicinity of the trailing edge of an upper surface blown flapFar-field noise data indicated that for practical upper surface blown flap configurations, the noise radiated below the flap is dominated by the noise generated in the vicinity of the trailing edge. Sound field by turbulent mixing in the trailing edge wake is investigated experimentally and theoretically. Hot-wire measurements were made downstream of the trailing edge to determine the gross turbulence mixing characteristics of the flow. This information is used as input to a theoretical analysis of the sound field. Favorable agreement is found between predicted and measured far-field noise directivities at various frequencies and noise power spectra at various directions.
Document ID
19760058412
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tam, C. K. W.
(Lockheed-Georgia Co., Marietta, Ga.; Florida State University Tallahassee, Fla., United States)
Reddy, N. N.
(Lockheed-Georgia Co. Marietta, Ga., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 76-503
Report Number: AIAA PAPER 76-503
Meeting Information
Meeting: Aero-Acoustics Conference
Location: Palo Alto, CA
Start Date: July 20, 1976
End Date: July 23, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A41378
Funding Number(s)
CONTRACT_GRANT: NAS1-13870
Distribution Limits
Public
Copyright
Other

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