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Modular Engine Noise Component Prediction System (MCP) Technical Description and Assessment DocumentThis report describes an empirical prediction procedure for turbofan engine noise. The procedure generates predicted noise levels for several noise components, including inlet- and aft-radiated fan noise, and jet-mixing noise. This report discusses the noise source mechanisms, the development of the prediction procedures, and the assessment of the accuracy of these predictions. Finally, some recommendations for future work are presented.
Document ID
20050186523
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Herkes, William H.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Reed, David H.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2005
Subject Category
Acoustics
Report/Patent Number
NASA/CR-2005-213526
Report Number: NASA/CR-2005-213526
Funding Number(s)
CONTRACT_GRANT: NAS1-97040
OTHER: 23-781-20-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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