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- W2182041431 abstract "A streamlined plate containing a rectangular cavity on one side was found to produce aerofoil tones. In the considered chordbased Reynolds number range of 1.0 × 10 5 to 1.8 × 10 5 , cavity oscillation modes did not occur due to insufficient cavity length (being 5% of chord). The discrete tonal frequencies showed good collapse with a U 0.85 scaling, suggesting that the tonal mechanism behaves similarly to that reported for smooth aerofoils. In this instance, the results suggest that an aeroacoustic feedback loop exists between the aerofoil trailing edge, where the noise is thought to be generated, and a highly receptive point in the boundary layer located at the cavity trailing edge. A region of separation near the aerofoil trailing edge is also believed to play a role in the amplification of the tones." @default.
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- W2182041431 date "2012-01-01" @default.
- W2182041431 modified "2023-09-27" @default.
- W2182041431 title "Aerofoil Tones Produced by a Streamlined Plate with Cavity" @default.
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