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Recent Progress in Engine Noise Reduction for Commercial Aircraft ApplicationsConsiderable progress has been made over the past ten years developing technologies for reducing aircraft noise. Engine noise continues to be a dominate source, particularly for aircraft departing from airports. Research efforts have concentrated on developing noise prediction methods, experimental validation, and developing noise reduction concepts that have been verified through model scale and static engine tests. Most of the work has concentrated on fan and jet components for commercial turbofan engines. In this seminar, an overview of the engine noise reduction work that was sponsored by NASA s Advanced Subsonic Technology Noise Reduction Program will be given, along with background information on turbofan noise sources and certification procedures. Concepts like "chevron" nozzles for jet noise reduction and swept stators for fan noise reduction will be highlighted. A preliminary assessment on how the new technologies will impact future engines will be given.
Document ID
20030112445
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Huff, Dennis L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Aircraft Design, Testing And Performance
Funding Number(s)
OTHER: 22-781-30-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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