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Core/Combustor Noise - Research OverviewContributions from the combustor to the overall propulsion noise of civilian transport aircraft are starting to become important due to turbofan design trends and advances in mitigation of other noise sources. Future propulsion systems for ultra-efficient commercial air vehicles are projected to be of increasingly higher bypass ratio from larger fans combined with much smaller cores, with ultra-clean burning fuel-flexible combustors. Unless effective noise-reduction strategies are developed, combustor noise is likely to become a prominent contributor to overall airport community noise in the future. This presentation gives a brief overview of the NASA outlook on pertinent issues and far-term research needs as well as current and planned research in the core/combustor-noise area. The research described herein is aligned with the NASA Ultra-Efficient Commercial Transport strategic thrust and is supported by the NASA Advanced Air Vehicle Program, Advanced Air Transport Technology Project, under the Aircraft Noise Reduction Subproject. The overarching goal of the Advanced Air Transport Technology (AATT) Project is to explore and develop technologies and concepts to revolutionize the energy efficiency and environmental compatibility of fixed wing transport aircrafts. These technological solutions are critical in reducing the impact of aviation on the environment even as this industry and the corresponding global transportation system continue to grow.
Document ID
20170005683
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Hultgren, Lennart S.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
June 21, 2017
Publication Date
April 11, 2017
Subject Category
Aeronautics (General)
Acoustics
Report/Patent Number
GRC-E-DAA-TN41435
Report Number: GRC-E-DAA-TN41435
Meeting Information
Meeting: Acoustics Technical Working Group (ATWG)
Location: Hampton, VA
Country: United States
Start Date: April 11, 2017
End Date: April 12, 2017
Funding Number(s)
WBS: WBS 081876.02.03.50.03.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Turbomachinery Noise
Aerocoustics
Combustor Noise
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