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Jet noiseThe main conclusions reached are: (1) At low subsonic jet exhaust velocities, jet noise varies as the velocity to the eighth power; (2) at high subsonic exhaust velocities, jet noise approaches a variation with velocity to the third power; (3) use of the jet density squared overcorrects density effects on jet noise; (4) subsonic and supersonic jet noise levels can be predicted; and (6) use of multielement nozzles and acoustically lined ejectors significantly suppress jet noise at intermediate jet exhaust velocities.
Document ID
19730003289
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vonglahn, U. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Gray, V. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Krejsa, E. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Lee, R. E., Jr.
(GE Cleveland, OH, United States)
Minner, G. L.
(NASA Lewis Research Center)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Aircraft Engine Noise Reduction
Subject Category
Aircraft
Accession Number
73N12016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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