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The Airframe Noise Reduction ChallengeThe NASA goal of reducing external aircraft noise by 10 dB in the near-term presents the acoustics community with an enormous challenge. This report identifies technologies with the greatest potential to reduce airframe noise. Acoustic and aerodynamic effects will be discussed, along with the likelihood of industry accepting and implementing the different technologies. We investigate the lower bound, defined as noise generated by an aircraft modified with a virtual retrofit capable of eliminating all noise associated with the high lift system and landing gear. However, the airframe noise of an aircraft in this 'clean' configuration would only be about 8 dB quieter on approach than current civil transports. To achieve the NASA goal of 10 dB noise reduction will require that additional noise sources be addressed. Research shows that energy in the turbulent boundary layer of a wing is scattered as it crosses trailing edge. Noise generated by scattering is the dominant noise mechanism on an aircraft flying in the clean configuration. Eliminating scattering would require changes to much of the aircraft, and practical reduction devices have yet to receive serious attention. Evidence suggests that to meet NASA goals in civil aviation noise reduction, we need to employ emerging technologies and improve landing procedures; modified landing patterns and zoning restrictions could help alleviate aircraft noise in communities close to airports.
Document ID
20040065977
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Lockard, David P.
(NASA Langley Research Center Hampton, VA, United States)
Lilley, Geoffrey M.
(Pennsylvania State Univ. State College, PA, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Subject Category
Acoustics
Report/Patent Number
NASA/TM-2004-213013
L-18346
Funding Number(s)
OTHER: 781-10-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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