4.7 Article

Broadband noise prediction for aerofoils with a serrated trailing edge based on Amiet's theory

期刊

JOURNAL OF SOUND AND VIBRATION
卷 512, 期 -, 页码 -

出版社

ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD
DOI: 10.1016/j.jsv.2021.116352

关键词

Trailing-edge noise; Computational aeroacoustics

资金

  1. EPSRC (Engineering and Physical Sciences Research Council) [EP/R029326/1]
  2. EPSRC [EP/R029326/1] Funding Source: UKRI

向作者/读者索取更多资源

This study examines the feasibility of using Amiet's theory to predict the noise reduction effect of serrated trailing edges, as well as improving prediction accuracy through directivity correction. Experimental results from wall-resolved large-eddy simulations show a significantly improved prediction with this correction method.
Trailing-edge serrations are used as means to reduce aerofoil broadband self-noise in various industrial applications. However, a reliable prediction of the reduced noise level has not been established to date. In this paper, the authors suggest that Amiet's theory can be used to accurately predict the sound radiated from serrated trailing edges. A plausible explanation as to how the classical theory, originally derived from non-serrated (straight) trailing edges, also works for the serrated trailing edges is provided. Besides, the authors propose a directivity correction to the Amiet's original model to account for realistic aerofoil geometry. The directivity correction provides a significantly improved prediction of the noise level in the upstream and downstream directions for both serrated and baseline trailing edge cases. This study is based on wall-resolved large-eddy simulations of Joukowski aerofoils with multiple serration geometries and in different flow conditions.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.7
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据