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Acoustic Efficiency of Azimuthal Modes in Jet Noise Using Chevron NozzlesThe link between azimuthal modes in jet turbulence and in the acoustic sound field has been examined in cold, round jets. Chevron nozzles, however, impart an azimuthal structure on the jet with a shape dependent on the number, length and penetration angle of the chevrons. Two particular chevron nozzles, with 3 and 4 primary chevrons respectively, and a round baseline nozzle are compared at both cold and hot jet conditions to determine how chevrons impact the modal structure of the flow and how that change relates to the sound field. The results show that, although the chevrons have a large impact on the azimuthal shape of the mean axial velocity, the impact of chevrons on the azimuthal structure of the fluctuating axial velocity is small at the cold jet condition and smaller still at the hot jet condition. This is supported by results in the azimuthal structure of the sound field, which also shows little difference in between the two chevron nozzles and the baseline nozzle in the distribution of energy across the azimuthal modes measured.
Document ID
20070003489
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Brown, Clifford A.
(NASA Glenn Research Center Cleveland, OH, United States)
Bridges, James
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
December 1, 2006
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2006-214364
AIAA Paper 2006-2654
E-15640
Report Number: NASA/TM-2006-214364
Report Number: AIAA Paper 2006-2654
Report Number: E-15640
Meeting Information
Meeting: 12th Aeroacoustics Conference
Location: Cambridge, MA
Country: United States
Start Date: May 8, 2006
End Date: May 10, 2006
Sponsors: Confederation of European Aerospace Societies, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 581.02.08.03.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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