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Parametric Testing of Chevrons on Single Flow Hot JetsA parametric family of chevron nozzles have been studied, looking for relationships between chevron geometric parameters, flow characteristics, and far-field noise. Both cold and hot conditions have been run at acoustic Mach number 0.9. Ten models have been tested, varying chevron count, penetration, length, and chevron symmetry. Four comparative studies were defined from these datasets which show: that chevron length is not a major impact on either flow or sound; that chevron penetration increases noise at high frequency and lowers it at low frequency, especially for low chevron counts; that chevron count is a strong player with good low frequency reductions being achieved with high chevron count without strong high frequency penalty; and that chevron asymmetry slightly reduces the impact of the chevron. Finally, it is shown that although the hot jets differ systematically from the cold one, the overall trends with chevron parameters is the same.
Document ID
20040152072
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Bridges, James
(NASA Glenn Research Center Cleveland, OH, United States)
Brown, Clifford A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2004
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2004-2824
NASA/TM-2004-213107
E-14582
Report Number: AIAA Paper 2004-2824
Report Number: NASA/TM-2004-213107
Report Number: E-14582
Meeting Information
Meeting: Tenth Aeroacoustics Conference
Location: Manchester
Country: United Kingdom
Start Date: May 10, 2004
End Date: May 12, 2004
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Funding Number(s)
WBS: WBS 22-781-30-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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