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首页> 外文期刊>Journal of Fluid Mechanics >On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction
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On the universal trends in the noise reduction due to wavy leading edges in aerofoil-vortex interaction

机译:在航空涡流相互作用中波浪前缘导致降噪的普遍趋势

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Existing studies suggest that wavy leading edges (WLEs) offer substantial reduction of broadband noise generated by an aerofoil undergoing upstream vortical disturbances. In this context, there are two universal trends in the frequency spectra of the noise reduction which have been observed and reported to date: (i) no significant reduction at low frequencies followed by (ii) a rapid growth of the noise reduction that persists in the medium-to-high frequency range. These trends are known to be insensitive to the aerofoil type and flow condition used. This paper aims to provide comprehensive understandings as to how these universal trends are formed and what the major drivers are. The current work is based on very-high-resolution numerical simulations of a semi-infinite flat-plate aerofoil impinged by a prescribed divergence-free vortex in an inviscid base flow at zero incidence angle, continued from recent work by the authors (Turner & Kim, J. Fluid Mech., vol. 811, 2017, pp. 582-611). One of the most significant findings in the current work is that the noise source distribution on the aerofoil surface becomes entirely two-dimensional (highly non-uniform in the spanwise direction as well as streamwise) at high frequencies when the WLE is involved. Also, the sources downstream of the LE make crucial contributions to creating the universal trends across all frequencies. These findings contradict the conventional LE-focused one-dimensional source analysis that has widely been accepted for all frequencies. The current study suggests that the universal trends in the noise-reduction spectra can be properly understood by taking the downstream source contributions into account, in terms of both magnitude and phase variations. After including the downstream sources, it is shown in this paper that the first universal trend is due to the conservation of total (surface integrated) source energy at low frequencies. The surface-integrated source magnitude that decreases faster with the WLE correlates very well with the noise-reduction spectrum at medium frequencies. In the meantime, the high-frequency noise reduction is driven almost entirely by destructive phase interference that increases rapidly and consistently with frequency, explaining the second universal trend.
机译:现有研究表明,波浪领先边缘(WLES)提供了由正在进行上游志性障碍的翼型产生的宽带噪声的大幅降低。在这种情况下,已经观察到并报告的降噪频谱有两个通用趋势:(i)在低频下没有显着降低,然后(ii)持续存在的降噪增长中高频率范围。已知这些趋势对所使用的空气型和流动条件不敏感。本文旨在为如何形成这些普遍趋势以及主要司机的方式提供全面的理解。目前的工作基于由零入射角的不可偏见的无源性涡流冲击的半无限平板空气罐的非常高分辨率数值模拟,从最近的作者继续由作者(Turner& Kim,J. Fluid Mech。,Vol.811,2017,PP。582-611)。当前工作中最重要的发现之一是在涉及WLE的高频时,空气涂层表面上的噪声源分布变得完全二维(在跨越方向上的高度不均匀)。此外,LE下游的来源为在所有频率上创造普遍趋势来说至关重要。这些发现与所有频率普遍接受的传统的le-ofe-ulidional源分析相矛盾。目前的研究表明,在幅度和相位变化方面,通过考虑下游源贡献,可以正确地理解降噪光谱的通用趋势。在包括下游来源之后,在本文中示出了第一普遍趋势是由于低频下的总(表面集成)源能量的源。通过在媒体频率下,通过WLE更快地与噪声降低频谱相比,表面集成源极限差异。同时,高频降噪几乎完全由破坏性相干扰驱动,从而随着频率迅速且始终如一地增加,解释了第二个普遍趋势。

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