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Control of Jet Noise Through Mixing EnhancementThe idea of using mixing enhancement to reduce jet noise is not new. Lobed mixers have been around since shortly after jet noise became a problem. However, these designs were often a post-design fix that rarely was worth its weight and thrust loss from a system perspective. Recent advances in CFD and some inspired concepts involving chevrons have shown how mixing enhancement can be successfully employed in noise reduction by subtle manipulation of the nozzle geometry. At NASA Glenn Research Center, this recent success has provided an opportunity to explore our paradigms of jet noise understanding, prediction, and reduction. Recent advances in turbulence measurement technology for hot jets have also greatly aided our ability to explore the cause and effect relationships of nozzle geometry, plume turbulence, and acoustic far field. By studying the flow and sound fields of jets with various degrees of mixing enhancement and subsequent noise manipulation, we are able to explore our intuition regarding how jets make noise, test our prediction codes, and pursue advanced noise reduction concepts. The paper will cover some of the existing paradigms of jet noise as they relate to mixing enhancement for jet noise reduction, and present experimental and analytical observations that support these paradigms.
Document ID
20030063290
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Bridges, James
(NASA Glenn Research Center Cleveland, OH, United States)
Wernet, Mark
(NASA Glenn Research Center Cleveland, OH, United States)
Brown, Cliff
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2003-212335
NAS 1.15:212335
E-13930
Meeting Information
Meeting: Noise-Con 2003
Location: Cleveland, OH
Country: United States
Start Date: June 23, 2003
End Date: June 25, 2003
Sponsors: Institute of Noise Control Engineering
Funding Number(s)
WBS: WBS 781-30-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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