Aeroacoustic source localization using the microphone array method with application to wind turbine noise

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2024-06-02 DOI:10.1177/1475472x241259122
Weicheng Xue, Bing Yang
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Abstract

The deconvolution DAMAS algorithm can effectively eliminate the misconceptions in the usually-used beamforming localization algorithm, allowing for a more accurate calculation of the source location as well as the intensity. When solving a linear system of equations, the DAMAS algorithm takes into account the mutual influence of different locations, reducing or even eliminating sidelobes and producing more accurate results. This work first introduces the principles of the DAMAS algorithm. Then it applies both the conventional beamforming algorithm and the DAMAS algorithm to simulate the localization of a single-frequency source from a 1.5 MW wind turbine, a complex line source with the text “UCAS” and a line source downstream of an airfoil trailing edge. Finally, the work presents experimental localization results of the source of a 1.5 MW wind turbine using both the conventional beamforming algorithm and the DAMAS algorithm.
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利用麦克风阵列法进行气声源定位,并应用于风力涡轮机噪声
解卷积 DAMAS 算法能有效消除通常使用的波束成形定位算法中的误解,从而更准确地计算出声源位置和强度。在求解线性方程组时,DAMAS 算法会考虑到不同位置的相互影响,从而减少甚至消除边扰,得出更精确的结果。这项工作首先介绍了 DAMAS 算法的原理。然后,它应用传统波束成形算法和 DAMAS 算法模拟了来自 1.5 兆瓦风力涡轮机的单频声源、带有 "UCAS "文字的复杂线声源和机翼后缘下游的线声源的定位。最后,作品展示了使用传统波束成形算法和 DAMAS 算法对 1.5 兆瓦风力涡轮机声源进行定位的实验结果。
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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