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Control of jet noiseThis reports describes experiments conducted at the High-Speed Jet Facility at the University of Southern California on supersonic jets. The goal of the study was to develop methods for controlling the noise emitted from supersonic jets by passive and/or active means. Work by Seiner et al (1991) indicates that eddy Mach wave radiation is the dominant noise source in a heated high speed jet. Eddy Mach radiation is caused by turbulent eddies traveling at supersonic speed in the shear layer of the jet. The convection velocity of the eddies decays with increasing distance from the nozzle exit due to the mixing of the jet stream with the ambient fluid. Once the convection speed reaches subsonic velocities, eddy Mach wave radiation ceases. To control noise, a rapid decay of the convection velocity is desired. This may be accomplished by enhanced mixing in the jet. In this study, small aspect ratio rectangular jet nozzles were tested. A flapping mode was noticed in the jets. By amplifying screech components of the jets and destabilizing the jet columns with a collar device, the flapping mode was excited. The result was a rapid decay of the jet velocity. A reduction in eddy Mach radiation in rectangular supersonic jets may be achieved with this device.
Document ID
19940006704
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Schreck, Stefan
(University of Southern California Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Acoustics
Report/Patent Number
NASA-CR-193612
NAS 1.26:193612
Report Number: NASA-CR-193612
Report Number: NAS 1.26:193612
Accession Number
94N11176
Funding Number(s)
CONTRACT_GRANT: NAG1-1096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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