NASA NTRS · 20050186523
Modular Engine Noise Component Prediction System (MCP) Technical Description and Assessment Document
Abstract
This 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.
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Herkes, William H., Reed, David H.. 2005-06-01. Modular Engine Noise Component Prediction System (MCP) Technical Description and Assessment Document. https://ntrs.nasa.gov/citations/20050186523
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