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Project TitleBFaNS
Track CodeLEW-17307
Websitehttp://www.grc.nasa.gov/WWW/Acoustics/analysis/support/broadband.htm
DescriptionThe broadband fan noise prediction system computes the broadband noise generated by the fan stage in a turbofan engine. The broadband noise sources consist of turbulence impinging on the leading edges of the fan and fan exit guide vane (FEGV), in addition to boundary layer turbulence convecting past the trailing edges.
AbstractNone
 
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