鸮翼后缘噪声的预测及控制

doi:10.13229/j.cnki.jdxbgxb201606030

吉林大学学报(工学版) ›› 2016, Vol. 46 ›› Issue (6): 1981-1986.doi: 10.13229/j.cnki.jdxbgxb201606030

鸮翼后缘噪声的预测及控制

葛长江¹, 叶辉¹, 胡兴军¹, 于征磊²

1.吉林大学汽车仿真与控制国家重点实验室,长春 130022;
2.吉林大学工程仿生教育部重点实验室,长春 130022

收稿日期:2015-11-12 出版日期:2016-11-20 发布日期:2016-11-20
作者简介:葛长江(1981-),男,工程师,博士.研究方向:工程仿生学.E-mail:163_gongbo@163.com
基金资助:
国家自然科学青年基金项目(51505182); 吉林省科技发展计划项目(20160520065JH)

Prediction and control of trailing edge noise on owl wings

GE Chang-jiang¹, YE Hui¹, HU Xing-jun¹, YU Zheng-lei²

1.State Key Laboratory of Automotive Simulation and Control, Jilin University, Changchun 130022, China;
2.Key Laboratory of Bionic Engineering, Ministry of Education, Jilin University, Changchun 130022, China

Received:2015-11-12 Online:2016-11-20 Published:2016-11-20

摘要/Abstract

摘要： 基于鸮翼的仿生翼型可用于揭示鸮翼的噪声产生机理。通过大涡模拟给出仿生翼型的流场,从中发现由前缘分离引起的两个声源分别为再附着的湍流边界层和从气泡中分离出来的涡脱落。由此可知,低雷诺数下的鸮翼宽频噪声是由湍流边界层散射导致的。之后,将被动多孔技术用于仿生翼型的后缘,在静压场中证实了多孔后缘缓解瞬态压力变化的作用。相关的噪声频谱也表明,多孔后缘具有高达10 dB以上的降噪潜力,但是降噪的幅度依赖于流阻率。

关键词: 工程仿生学, 仿生翼型, 涡脱落, 湍流边界层, 多孔处理, 后缘降噪

Abstract: An airfoil mimicking owl wings is used to determine the noise generation mechanism of silent owl. The flow field around the bionic airfoil suggests two noise sources caused by the leading-edge separation, one is the reattached turbulent boundary and the other one is the vortex shedding detached from leading-edge bubble. The reason for owl wing noise in low Reynolds number is the interaction between the turbulent boundary layer and the sharp trailing-edge of the bionic airfoil. Furthermore, as a promising means, the passive porosity technology is applied for the trailing-edge noise reduction of the airfoil. The static pressure fields around the airfoil verify that the porous trailing-edge can alleviate pressure change by the suppression of the vortex shedding and the damping of broadband turbulent boundary layer fluctuation. The relevant noise spectrum also indicates a pronounced noise reduction potential in excess of 10 dB, but in dependence on the flow resistivity. The findings of this study may be used as reference in the design of silent aircraft.

Key words: engineering bionics, bionic airfoil, vortex shedding, turbulent boundary layer, porous treatment, trailing edge noise reduction

中图分类号:

TB17

葛长江, 叶辉, 胡兴军, 于征磊. 鸮翼后缘噪声的预测及控制[J]. 吉林大学学报(工学版), 2016, 46(6): 1981-1986.

GE Chang-jiang, YE Hui, HU Xing-jun, YU Zheng-lei. Prediction and control of trailing edge noise on owl wings[J]. 吉林大学学报(工学版), 2016, 46(6): 1981-1986.

参考文献

[1] Takeda K, Ashcroft G B, Zhang X. Unsteady aerodynamics of slat cove flow in a high-lift device configuration[C]∥AIAA Paper, 2001-0706.
[2] Graham R R. The silent flight of owls[J]. J R Aeronaut,1934,38:837-843.
[3] Lilley G M. A study of the silent flight of the owl[J]. AIAA Paper, 1998-2340.
[4] Chen K,Liu Q P,Liao G H,et al. The sound suppression characteristics of wing feather of owl (Bubo bubo)[J]. Journal of Bionic Engineering, 2012,9(2):192-199.
[5] Herr M. New Results in Numerical and Experimental Fluid Mechanics V: Experimental Study on Noise Reduction through Trailing Edge Brushes[M]. Berlin Heidelberg:Springer, 2006:365-372.
[6] Tinetti A F, Kelly J F, Bauer S X S, et al. On the use of surface porosity to reduce unsteady lift[C]∥AIAA Paper, 2001-2921.
[7] Tinetti A F,Kelly J F,Thomas R H,et al. Reduction of wake-stator interaction noise using passive porosity[C]∥AIAA Paper,2002-1036.
[8] Sarradj E, Geyer T. Noise generation by porous airfoils[J]. AIAA Paper, 2007-3719.
[9] Geyer T, Sarradj E, Fritzsche C. Porous airfoils: noise reduction and boundary layer effects[C]∥AIAA Paper,2009-3392.
[10] Sueki T, Ikeda M, Takaishi T. Aerodynamic noise reduction using porous materials and their application to high-speed pantographs[R]. Quarterly Report of RTRI,2009,50(1):26-31.
[11] Marsden A L, Wang M, Dennis J E, et al. Trailing-edge noise reduction using derivative-free optimization and large-eddy simulation[J]. Journal of Fluid Mechanics,2007,572:13-36.
[12] Lai H X, Luo K H. A conceptual study of cavity aeroacoustics control using porous media inserts[J]. Flow Turbul Combust,2008,80(3):375-391.
[13] Bruneau C H, Mortazavi I. Numerical modelling and passive flow control using porous media[J]. Comput Fluids,2008,37(5):488-498.
[14] Frink N, Bonhaus D, Vatsa V, et al. A boundary condition for simulation of flow over porous surfaces[J]. AIAA Paper,2001-2412.
[15] Khorrami M R, Li F, Choudhari M. Novel approach for reducing rotor tip clearance-induced noise in turbofan engines[J]. AIAA Journal,2002,40(8):1518-1528.
[16] 任露泉,孙少明,徐成宇. 鸮翼前缘非光滑形态消声降噪机理[J]. 吉林大学学报:工学版,2008,38(增刊1):126-131.
Ren Lu-quan,Sun Shao-ming,Xu Cheng-yu. Noise reduction mechanism of non-smooth leading edge of owl wing[J]. Journal of Jilin University(Engineering and Technology Edition), 2008,38(Sup.1):126-131.
[17] Klan S, Bachmann T, Klaas M, et al. Experimental analysis of the flow field over a novel owl based airfoil[J]. Experiments in Fluids,2009,46(5):975-989.
[18] Ge C J, Ren L Q, Liang P, et al. High-lift effect of bionic slat based on owl wing[J]. Journal of Bionic Engineering,2013,10(4):456-463.
[19] Geyer T, Sarradj E, Fritzsche C. Measurement of the noise generation at the trailing edge of porous airfoils[J]. Experiments in Fluids,2010,48(2):291-308.
[20] Arcondoulis E J G, Doolan C J, Zander A C, et al. On the generation of airfoil tonal noise at zero angle of attack and low to moderate Reynolds number[J]. AIAA Paper,2012-2060.
[21] Herr M, Dobrzynski W. Experimental investigation in low-noise trailing edge design[C]∥AIAA Paper, 2004-2804.

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鸮翼后缘噪声的预测及控制

Prediction and control of trailing edge noise on owl wings

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