Exploring the suppression mechanism of wind buffeting noise with bionic structures featuring leading-edge serrations and surface ridges

IF 2.8 4区 工程技术 Q1 ACOUSTICS Journal of Low Frequency Noise Vibration and Active Control Pub Date : 2023-06-21 DOI:10.1177/14613484231185416
S. Cao, Zhifei Zhang, Xiong Wu, Yansong He, Quanzhou Zhang
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Abstract

The aim of this study is to investigate the effectiveness and mechanism of wind buffeting noise suppression using a new bionic structure inspired by the quiet flight of owls. Firstly, the new bionic schemes based on NACA0012 wing with two sinusoidal leading-edge serrations and one straight leading-edge curve are used in a cavity after verifying the simulation. Then, the results of the three bionic schemes are compared and analyzed. It is found that the schemes with leading-edge serrations and surface ridges can suppress wind buffeting noise effectively. In particular, the sinusoidal scheme with a wavelength λ = 0.24 c (chord length c) can significantly reduce resonance energies above 21 dB over a wide range of speeds. Furthermore, the study reveals that in the bionic scheme, only the negative pressure core moves in the opening and hits the trailing edge, which reduces the pressure fluctuation in the cavity. The boundary layer thickness (BLT) also fluctuates in span under the influence of the leading-edge serration and the surface ridge, which is favorable for suppressing wind buffeting noise. However, the suppression effect is not solely related to the fluctuation of BLT in the span at the trailing edge but is also influenced by the minimum BLT at this point. Therefore, if the BLT has a certain intensity fluctuation in the span, and the minimum BLT at the trailing edge is close to that of the smooth airfoil scheme, the noise suppression effect is significant.
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利用前缘锯齿和表面脊状仿生结构探索风抖振噪声的抑制机制
本研究的目的是利用一种受猫头鹰安静飞行启发的新型仿生结构来研究风振噪声抑制的有效性和机制。首先,将基于NACA0012机翼的两种正弦前缘锯齿和一种直线前缘曲线的仿生方案在空腔中进行仿真验证。然后,对三种仿生方案的结果进行了比较分析。结果表明,采用前缘锯齿和表面脊的方案可以有效地抑制风抖振噪声。特别是,波长λ = 0.24 c(弦长c)的正弦方案可以在很宽的速度范围内显著降低21 dB以上的共振能量。此外,研究表明,在仿生方案中,只有负压芯在开口中移动并撞击尾缘,从而减小了腔内的压力波动。边界层厚度在前缘锯齿和表面脊的影响下呈跨幅波动,有利于抑制风抖振噪声。然而,抑制效果不仅与尾缘跨度内叶压t的波动有关,还受该点最小叶压t的影响。因此,如果翼型在跨度上有一定的强度波动,且尾缘处的最小翼型与光滑翼型方案的最小翼型接近,则噪声抑制效果显著。
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来源期刊
CiteScore
4.90
自引率
4.30%
发文量
98
审稿时长
15 weeks
期刊介绍: Journal of Low Frequency Noise, Vibration & Active Control is a peer-reviewed, open access journal, bringing together material which otherwise would be scattered. The journal is the cornerstone of the creation of a unified corpus of knowledge on the subject.
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