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Trailing edge noise data with comparison to theoryThe noise emission generated by the passage of a turbulent airstream over the trailing edge of a semi-infinite plate was measured over a large range of airstream velocity and plate geometry. The experiment was designed to validate trailing edge noise theories. The results show that the peak of the radiation pattern moves from an upstream to a downstream direction as the velocity increases. The measured radiation pattern of the noise was in excellent agreement with that predicted by the recent theory of Goldstein. As predicted, the pattern shape was independent of the nature of the turbulence producing the noise.
Document ID
19790019759
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olsen, W.
(NASA Lewis Research Center Cleveland, OH, United States)
Boldman, D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Acoustics
Report/Patent Number
E-093
AIAA PAPER 79-1524
NASA-TM-79208
Report Number: E-093
Report Number: AIAA PAPER 79-1524
Report Number: NASA-TM-79208
Meeting Information
Meeting: Fluid and Plasma Dynamics Conf.
Location: Williamsburg, VA
Country: United States
Start Date: July 23, 1979
End Date: July 25, 1979
Sponsors: AIAA
Accession Number
79N27930
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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