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- W2314663183 abstract "Acoustic treatment in aeroengine nacelle is an esse ntial part of the overall aircraft noise reduction effort. Especially with the increase of b ypass ratio of civil transport turbofans, the contribution of fan to the overall noise will be fu rther enhanced. Nowadays, in the outlet nacelle of a turbofan engine with high bypass ratio the fan/rotor rotation will definitely generate a mean swirling flow, especially between t he rotor and stator where the azimuthal velocity component could even be comparable to the axial component. However, the effect of mean swirl on the sound transmission characteristics has not been paid more attention to until recently due to the complex computational model and the restriction of computer in presence of mean swirl. That had been study in this paper. Nomenclature Γ = strength of free vortex Ω = angular velocity θ M = Mach number of the swirling flow r = radius m r = average radius T r = tip radius final M = Mach number u M = Mach number of the axial flow r M = Mach number of the radial flow" @default.
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- W2314663183 date "2010-06-07" @default.
- W2314663183 modified "2023-09-23" @default.
- W2314663183 title "The Measurement of Mean Flow of Fan and Its Effect on the Liner Design" @default.
- W2314663183 cites W2076583044 @default.
- W2314663183 doi "https://doi.org/10.2514/6.2010-3831" @default.
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