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PIV/Phased Array/Far-Field Noise Measurements of a Low-Noise Top-Mounted Propulsion Installation for a Supersonic AirlinerA model-scale exhaust system was tested to validate low-noise concepts and noise prediction methods. The tests involved far-field acoustics, translating phased array, and particle image velocimetry; this report covers the far-field acoustic measurements. Data were acquired for a series of nozzles with different chevron designs, both uninstalled and installed on a representative aircraft planform. The impact of the various chevron treatments on the far-field noise was documented, along with the impact of the pylon and planform. For the baseline nozzle, installation produced a 2 EPNdB (Effective Perceived Noise in deciBels) reduction, as assumed in system studies. Chevrons were used to shift noise sources upstream to maximize the installation benefits and to reduce unshielded sources downstream. These resulted in reductions of 4-5 EPNdB...
Document ID
20190025420
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Bridges, James
(NASA Glenn Research Center Cleveland, OH, United States)
Cluts, Jordan
(NASA Glenn Research Center Cleveland, OH, United States)
Podboy, Gary
(NASA Glenn Research Center Cleveland, OH, United States)
Wernet, Mark
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
May 30, 2019
Publication Date
April 10, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN67394
Meeting Information
Meeting: Acoustics Technical Working Group (ATWG) Spring 2019 Meeting
Location: Hampton, VA
Country: United States
Start Date: April 10, 2019
End Date: April 12, 2019
Sponsors: NASA Langley Research Center
Funding Number(s)
WBS: 110076.02.03.04.40.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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