An Analytic Solution for the Noise Generated by Gust-Aerofoil Interaction for Plates with Serrated Leading Edges
Lorna J Ayton, Jae Wook Kim

TL;DR
This paper develops an analytical solution for noise generated by gust interaction with serrated-edged plates, revealing mechanisms for noise reduction and matching experimental and numerical results.
Contribution
It introduces an analytic approach using Wiener-Hopf method to model gust-plate interaction with serrated edges, providing insights into noise reduction mechanisms.
Findings
Logarithmic relation between serration height and noise decrease
Destructive interference as a noise reduction mechanism
Good agreement with experimental and numerical data
Abstract
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 background steady uniform flow. Viscous and non-linear effects are neglected. The Wiener-Hopf method is used in conjunction with a non-orthogonal coordinate transformation and separation of variables to permit analytical progress. The solution is obtained in terms of a modal expansion in the spanwise coordinate, however for low- and mid-range incident frequencies only the zeroth order mode is seen to contribute to the far-field acoustics, therefore the far-field noise can be quickly evaluated. The solution gives insight into the potential mechanisms behind the reduction of noise for plates with serrated leading edges compared to those with straight edges, and predicts a logarithmic dependence between the tip-to-root serration…
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