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A review of airfoil trailing edge noise with some implications for wind turbines

机译:机翼后缘噪声的研究对风力涡轮机有一些影响

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As trailing edge noise is the major aerodynamic noise source on a wind turbine, it is timely and relevant to review previous work in this area. This paper presents a review of previous experimental trailing edge noise studies and compares available experimental noise data for the NACA 0012 profile with data from two numerical studies. The literature review and comparison reveal the extent of the data available, the scatter in the results and some of the ideas about the cause of the scatter. Noise data compare well at laboratory scale Reynolds numbers; however, at higher Reynolds numbers that are comparable to large wind turbines, there is not much agreement and the published data are limited. Resolution of the peak radiating frequency and level must be improved in order to improve the accuracy of wind turbine noise predictions. To do so requires new experimental and computational research to understand the noise generating physics in better detail.
机译:由于后缘噪声是风力涡轮机上的主要空气动力学噪声源,因此回顾该领域的先前工作是及时且相关的。本文介绍了以前的实验后沿噪声研究的概况,并将NACA 0012轮廓的可用实验噪声数据与两个数值研究的数据进行了比较。文献综述和比较揭示了可用数据的范围,结果中的分散以及有关分散原因的一些想法。噪声数据在实验室规模的雷诺数下可以很好地比较;但是,在雷诺数更高(可与大型风力涡轮机相媲美)的情况下,达成的共识并不多,而且公布的数据有限。为了提高风力涡轮机噪声预测的准确性,必须提高峰值辐射频率和水平的分辨率。为此,需要进行新的实验和计算研究,以更详细地了解产生噪声的物理原理。

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