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Bibliographic Details
Main Authors: Xue, Weicheng, Jia, Shaohong, Wang, Hongyu, Chen, Zhe, Yang, Bing
Format: Preprint
Published: 2023
Subjects:
Online Access:https://arxiv.org/abs/2307.12188
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author Xue, Weicheng
Jia, Shaohong
Wang, Hongyu
Chen, Zhe
Yang, Bing
author_facet Xue, Weicheng
Jia, Shaohong
Wang, Hongyu
Chen, Zhe
Yang, Bing
contents This study explores the noise reduction achieved by airfoils with serrated trailing edges in a low turbulence wind tunnel, focusing on acoustic spectral characteristics and wake flow field measurements. We analyze the effects of various factors, including Reynolds number, angle of attack, serration parameters, and model type, on sound power levels and far-field radiation patterns. Our findings reveal that serrated trailing edges significantly reduce blunt vortex shedding noise and laminar separation bubble noise across a broader frequency range, particularly in the mid-to-high frequency range, with reductions delineated by two boundaries. Interestingly, the serration geometry exhibits minimal impact on noise reduction, which varies with the angle of attack and airfoil profile across all tested conditions. Additionally, while serrations effectively lower noise levels, especially at higher frequencies, they do not significantly alter the airfoil's acoustic directivity patterns. Measurements of wake flow velocity spectra demonstrate a clear correlation between reduced wake turbulence and noise reduction, as serrated edges decrease the power spectral density of turbulent velocity fluctuations, effectively disrupting larger vortex structures responsible for noise generation. These valuable insights contribute to understanding the acoustic benefits of serrated trailing edges.
format Preprint
id arxiv_https___arxiv_org_abs_2307_12188
institution arXiv
publishDate 2023
record_format arxiv
spellingShingle An Experimental Study of Noise Reduction in Wind Turbine Airfoils with Serrated Trailing Edges
Xue, Weicheng
Jia, Shaohong
Wang, Hongyu
Chen, Zhe
Yang, Bing
Fluid Dynamics
This study explores the noise reduction achieved by airfoils with serrated trailing edges in a low turbulence wind tunnel, focusing on acoustic spectral characteristics and wake flow field measurements. We analyze the effects of various factors, including Reynolds number, angle of attack, serration parameters, and model type, on sound power levels and far-field radiation patterns. Our findings reveal that serrated trailing edges significantly reduce blunt vortex shedding noise and laminar separation bubble noise across a broader frequency range, particularly in the mid-to-high frequency range, with reductions delineated by two boundaries. Interestingly, the serration geometry exhibits minimal impact on noise reduction, which varies with the angle of attack and airfoil profile across all tested conditions. Additionally, while serrations effectively lower noise levels, especially at higher frequencies, they do not significantly alter the airfoil's acoustic directivity patterns. Measurements of wake flow velocity spectra demonstrate a clear correlation between reduced wake turbulence and noise reduction, as serrated edges decrease the power spectral density of turbulent velocity fluctuations, effectively disrupting larger vortex structures responsible for noise generation. These valuable insights contribute to understanding the acoustic benefits of serrated trailing edges.
title An Experimental Study of Noise Reduction in Wind Turbine Airfoils with Serrated Trailing Edges
topic Fluid Dynamics
url https://arxiv.org/abs/2307.12188