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Acoustic properties of a supersonic fanTests of supersonic rotors designed to reduce forward propagating pressure waves and the accompanying blade passing tones and multiple pure tones showed the wave propagation and noise reduction to have been obtained at the expense of increased noise radiation rearward. Outlet guide vanes served to muffle the noise propagating rearwards, but did not affect forward propagation at all.
Document ID
19730006298
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Goldstein, A. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Glaser, F. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Coats, J. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-7096
E-6953
Report Number: NASA-TN-D-7096
Report Number: E-6953
Accession Number
73N15025
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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