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Program Predicts Broadband Noise from a Turbofan EngineBroadband Fan Noise Prediction System (BFaNS) is a computer program that, as its name indicates, predicts the broadband noise generated by the fan stage of a turbofan engine. This noise is the sum of (1) turbulent-inflow noise, which is caused by turbulence impinging on leading edges of the fan and the fan exit guide vane and (2) self noise, which is caused by turbulence convecting past the corresponding trailing edges. The user provides input data on the fan-blade, vane, and flow-path geometries and on the mean and turbulent components of the flow field. BFaNS then calculates the turbulent-inflow noise by use of D. B. Hanson's theory, which relates sound power to the inflow turbulence characteristics and the cascade geometry. Hanson s program, BBCASCADE, is incorporated into BFaNS, wherein it is applied to the rotor and stator in a stripwise manner. The spectra of upstream and downstream sound powers radiated by each strip are summed to obtain the total upstream and downstream sound-power spectra. The self-noise contributions are calculated by S. A. L. Glegg's theory, which is also applied in a stripwise manner. The current version of BFaNS is limited to fans with subsonic tip speeds.
Document ID
20110016562
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
Authors
Morin, Bruce L.
(United Technologies Corp. Wright-Patterson AFB, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2004
Publication Information
Publication: NASA Tech Briefs, January 2004
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LEW-17307
Distribution Limits
Public
Copyright
Public Use Permitted.
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