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An MDOE Assessment of Nozzle Vanes for High Bypass Ratio Jet Noise ReductionThe effect of airfoil-shaped vanes placed in the fan stream of a BPR 8 coannular nozzle model system on the resulting jet noise was investigated. The experiments used a Modern Design of Experiments approach to investigate the impact of a range of vane parameters on the noise reduction achieved at representative takeoff conditions. The experimental results showed that the installation of the vanes decreased low frequency noise radiation in the downstream peak-noise direction and increased high frequency noise in the upstream direction. Results also showed that improper selection of the vane configuration resulted in increased low frequency noise radiation in the upstream direction. Large angles of attack are shown to reduce noise near the peak jet noise angle and increase noise in the upstream direction. The MDOE analysis yields an optimum design that minimizes perceived noise levels. Limited data taken with a BPR 5 nozzle system showed that the vanes result in better effective perceived noise reduction for lower bypass ratio nozzles than for the BPR 8 model.
Document ID
20060018357
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Henderson, Brenda
(NASA Langley Research Center Hampton, VA, United States)
Norum, Thomas
(NASA Langley Research Center Hampton, VA, United States)
Bridges, James
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2006
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2006-2543
Meeting Information
Meeting: 12th AIAA/CEAS Aeroacoustics Conference
Location: Cambridge, MA
Country: United States
Start Date: May 8, 2006
End Date: May 10, 2006
Sponsors: American Inst. of Aeronautics and Astronautics, National Oceanic and Atmospheric Administraion
Funding Number(s)
OTHER: 23-781-30-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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