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Low-frequency rear quadrant noise of a turbojet engine with exhaust duct mufflingA J-65 engine was run with a tuned sound-absorbing exhaust duct to study the internal and jet components of rear quadrant noise. Full muffler, hard wall duct, and regular production engine configurations were tested. The jet exhaust velocities were subsonic. The use of the exhaust muffler extended the relation between the jet noise and the eighth power of the jet velocity to lower velocities than for the hard wall duct.
Document ID
19730007284
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Woodward, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Minner, G. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Aircraft
Report/Patent Number
E-7202
NASA-TM-X-2718
Report Number: E-7202
Report Number: NASA-TM-X-2718
Accession Number
73N16011
Funding Number(s)
PROJECT: RTOP 501-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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