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Recent Progress in Aircraft Noise ResearchAn overview of the acoustics research at NASA under the Subsonic Fixed Wing project is given. The presentation describes the rationale behind the noise reduction goals of the project in the context of the next generation air transportation system, and the emphasis placed on achieving these goals through a combination of the in-house and collaborative efforts with industry, universities and other government agencies. The presentation also describes the in-house research plan which is focused on the development of advanced noise and flow diagnostic techniques, next generation noise prediction tools, and novel noise reduction techniques that are applicable across a wide range of aircraft.
Document ID
20080006600
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Envia, Edmane
(NASA Glenn Research Center Cleveland, OH, United States)
Thomas, Russell
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
October 16, 2007
Subject Category
Aerodynamics
Meeting Information
Meeting: Fundamental Aeronautics Annual Meeting
Location: New Orleans, LA
Country: United States
Start Date: October 30, 2007
End Date: November 1, 2007
Funding Number(s)
WBS: WBS 561581.02.08.03.18.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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