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An analytic solution for gust-aerofoil interaction noise for plates with leading-edge serrations

机译:锯齿状前沿板的翼型-翼型相互作用噪声的解析解

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This paper presents an analytic solution for the sound generated by an unsteady gust interacting with a semi-infinite flat plate with a serrated leading edge in a channel. The Wiener-Hopf method is used in conjunction with a non-orthogonal coordinate transformation to allow analytical progress. A solution is obtained in terms of a modal expansion, however for low- and mid-range incident frequencies only the zeroth order mode contributes to the far-field acoustics. When this is the case it is found that the modal expansion terms can be replaced by a closed-form expression that is independent of the modal expansion, allowing very quick evaluation in both the far-field and on the surface, and eliminates the possibility of Gibbs phenomenon influencing the solution. The solution gives insight into the potential mechanisms behind the reduction of noise for serrations compared with that from a straight edge.
机译:本文针对不稳定的阵风与通道中带有锯齿状前缘的半无限平板相互作用而产生的声音提出了一种解析解决方案。 Wiener-Hopf方法与非正交坐标转换结合使用以允许进行分析。可以通过模态扩展获得解决方案,但是对于中低频入射频率,只有零阶模有助于远场声学。在这种情况下,可以发现模态扩展项可以由独立于模态扩展的闭式表达式代替,从而可以在远场和表面上非常快速地进行评估,并消除了吉布斯现象影响解决方案。该解决方案使您可以深入了解锯齿状噪声与直线边缘噪声相比背后的潜在机制。

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