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- W2187843101 abstract "Rotor-stator interaction has been identified as the dominant noise source of a vertical take-off and landing (VTOL) aircraft developed by Entecho. This paper reports field measurement results of blade passing noise of the VTOL aircraft together with its analysis and control. The blade passing event was simulated in a wind tunnel experiment. The flow speed, rotor position and rotor-stator spacing were varied with the chord-wise pressure distribution of the leading surface of the rotor blade being measured by an array of 6 flush mounted microphones. Results show useful features of the pressure distribution on the rotor blade influenced by an up stream stator, which are used for the analysis and prediction of the sound radiation from the VTOL aircraft. The preliminary result of the reduction of the blade passing noise using angled stator blades is also presented." @default.
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- W2187843101 date "2009-01-01" @default.
- W2187843101 modified "2023-09-22" @default.
- W2187843101 title "Analysis and reduction of blade passing noise of a VTOL aircraft" @default.
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- W2187843101 hasPublicationYear "2009" @default.
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