Utilization of Whale-inspired Leading-edge Tubercles for Airfoil Noise Reduction

被引:2
|
作者
Chen, Weijie [1 ]
Zhang, Liangji [1 ]
Wang, Liangfeng [2 ]
Wei, Zuojun [3 ]
Qiao, Weiyang [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Peoples R China
[2] High Speed Aerodynam Inst, China Aerodynam Res & Dev Ctr, Mianyang 621000, Sichuan, Peoples R China
[3] Southern Univ Sci & Technol, Dept Mech & Aerosp Engn, Shenzhen 518055, Peoples R China
基金
中国国家自然科学基金;
关键词
Bionic design; Humpback whale; Leading-edge tubercle; Large eddy simulation; Noise reduction mechanism; AEROFOIL INTERACTION; PERFORMANCE; PREDICTION; SERRATIONS;
D O I
10.1007/s42235-022-00210-3
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Numerical studies are conducted to explore the noise reduction effect of leading-edge tubercles inspired by humpback whale flippers. Large eddy simulations are performed to solve the flow field, while the acoustic analogy theory is used for noise prediction. In this paper, a baseline airfoil with a straight leading-edge and three bionic airfoils with tubercled leading-edges are simulated. The tubercles have sinusoidal profiles and the profiles are determined by the tubercle wavelength and amplitude. The tubercles used in this study have a fixed wavelength of 0.1c with three different amplitudes of 0.1c, 0.15c and 0.2c, where c is the mean chord of the airfoil. The freestream velocity is set to 40 m/s and the chord based Reynolds number is 400,000. The predicted flow field and acoustic field of the baseline airfoil are compared against the experiments and good agreements are found. A considerable noise reduction level is achieved by the leading-edge tubercles and the tubercle with larger amplitude can obtain better noise reduction. The underlying flow mechanisms responsible for the noise reduction are analyzed in detail.
引用
收藏
页码:1405 / 1421
页数:17
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