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Velocity measurements in a turbulent trailing vortex and their application to BWI noise predictionThe objectives were to observe the turbulence structure and spectral characteristics of the trailing vortex shed by a rectangular NACA 0012 wing over a range of conditions and to incorporate these observations into the blade-wake interaction (BWI) noise-prediction method of Glegg (1989). The following sections are presented: (1) measurements performed during the first year of this two year investigation; (2) presentation and discussion of a representative sample of the results; (3) implications for the BWI noise prediction method; and (4) re-evaluation of work planned for the second year.
Document ID
19910011787
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Devenport, William J.
(Virginia Polytechnic Inst. Blacksburg., United States)
Glegg, Stewart A. L.
(Florida Atlantic Univ. Boca Raton., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-188083
NAS 1.26:188083
Report Number: NASA-CR-188083
Report Number: NAS 1.26:188083
Accession Number
91N21100
Funding Number(s)
CONTRACT_GRANT: NAG1-1119
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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