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柔性薄板翼流固耦合振动噪声风洞试验研究
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  • 英文篇名:Wind tunnel experimental study on noise of flexible thin plate wing with fluid-solid interaction effects
  • 作者:曹亮 ; 杨鹏飞 ; 王怡星 ; 陈刚
  • 英文作者:CAO Liang;YANG PengFei;WANG Yi Xing;CHEN Gang;State Key Laboratory for Strength and Vibration of Mechanical Structures, Shannxi Key Laboratory of Environment and Control for Flight Vehicle,School of Aerospace, Xi'an Jiaotong University;
  • 关键词:流固耦合 ; 气动噪声 ; 声学风洞试验 ; 柔性薄板翼
  • 英文关键词:fluid-solid interaction;;aeroacoustics;;acoustics wind tunnel;;flexible thin plate wing
  • 中文刊名:JEXK
  • 英文刊名:Scientia Sinica(Technologica)
  • 机构:西安交通大学航天航空学院机械结构强度与振动国家重点实验室西安交通大学声学风洞实验室;
  • 出版日期:2018-12-03 17:01
  • 出版单位:中国科学:技术科学
  • 年:2019
  • 期:v.49
  • 基金:国家自然科学基金(批准号:11672225,11872293,11472206,11371288);; 气动噪声控制重点实验室开放基金(编号:1801ANCL20180103)资助
  • 语种:中文;
  • 页:JEXK201907007
  • 页数:10
  • CN:07
  • ISSN:11-5844/TH
  • 分类号:79-88
摘要
柔性结构在风场中会发生流固耦合振动,其噪声特性要比流场中刚性结构气动噪声更为复杂.通过声学风洞试验,对比研究了流固耦合作用下不同柔性薄板翼模型的气动噪声特性.试验表明,随着结构柔性增加,薄翼气动噪声声压级对风速和迎角变化更加敏感.柔性平板翼噪声的频谱特性和声源位置都与刚性翼明显不同.研究发现,在特定迎角和风速下气动噪声强度会突然显著增强.给出了流固耦合作用下的平板翼气动噪声变化初步规律,为相关流固耦合振动噪声理论分析和数值模拟提供了试验支撑.
        The flexible structure may generate fluid-structure coupled vibration in the wind field. At this time its noise characteristics are more complicated than the aeroacoustics of the rigid structure in the flow field. Through the acoustic wind tunnel test, the noise characteristics of different flexible thin plate-wing models under fluid were studied. Experiments show that with the increase of structural flexibility, the OASPL of the thin wing is more sensitive to changes of wind speed and angle of attack. The spectral characteristics and sound source position of the flexible plat-wing noise are obviously different from that of the rigid wing. The study found that the aeroacoustic intensity suddenly and remarkably increases at a specific angle of attack and wind speed. The preliminary law of the aeroacoustics variation of the plate-wing under the fluid-solid coupling is given, which provides the experimental support for the theoretical analysis and numerical simulation of the relevant fluid-structure coupled vibration noise.
引文
1 Wang M,Freund J B,Lele S K.Computational prediction of flow-generated sound.Annu Rev Fluid Mech,2006,38:483-512
    2王晶.薄翼型叶片仿生流动控制降噪及其应用研究.博士学位论文.长春:吉林大学,2017
    3 Williams J E F,Hall L H.Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane.J Fluid Mech,1970,40:657-670
    4 Brooks T F,Pope D S,Marcolini M A.Airfoil self-noise and prediction.NASA Technical Report NASA-RP-1218.1989
    5 Archibald F S.The laminar boundary layer instability excitation of an acoustic resonance.J Sound Vib,1975,38:387-402
    6 Choudhari M M,Lockard D P,Macaraeg M G,et al.Aeroacoustic experiments in the NASA Langley low-turbulence pressure tunnel.NASATechnical Report NASA/TM-2002-211432.2002
    7 Ovenden N C,Rienstra S W.Mode-matching strategies in slowly varying engine ducts.AIAA J,2004,42:1832-1840
    8 Sarradj E,Geyer T.Noise generation by porous airfoils.In:13th AIAA/CEAS Aeroacoustics Conference.Rome,2007
    9 Herr M,Dobrzynski W.Experimental investigations in low-noise trailing edge design.AIAA J,2005,43:1167-1175
    10 Herr M.Design Criteria for low-noise trailing-edges.In:13th AIAA/CEAS Aeroacoustics Conference.Rome,2007
    11 Finez A,Jacob M,Roger M,et al.Broadband noise reduction of linear cascades with trailing edge serrations.In:17th AIAA/CEAS Aeroacoustics Conference.Portland,2013
    12 Howe M S.Noise produced by a sawtooth trailing edge.J Acoust Soc Am,1991,90:482-487
    13仝帆,乔渭阳,王良锋,等.仿生学翼型尾缘锯齿降噪机理.航空学报,2015,36:2911-2922
    14 Wu S F,Maestrello L.Responses of finite baffled plate to turbulent flow excitations.AIAA J,1995,33:13-19
    15 Howe M S.Sound produced by an aerodynamic source adjacent to a partly coated,finite elastic plate.Proc R Soc A-Math Phys Eng Sci,1992,436:351-372
    16 Graham W R.Boundary layer induced noise in aircraft,part I:The flat plate model.J Sound Vib,1996,192:101-120
    17 Tang S K,Leung R C K,So R M C,et al.Acoustic radiation by vortex induced flexible wall vibration.J Acoust Soc Am,2005,118:2182-2189
    18 Sch?fer F,Müller S,Uffinger T,et al.Fluid-structure-acoustic interaction of the flow past a thin flexible structure.AIAA J,2010,48:738-748
    19 Purohit A,Darpe A K,Singh S P.A study on aerodynamic sound from an externally excited flexible structure in flow.Comput Fluids,2014,103:100-115
    20 Bae Y,Jang J Y,Moon Y J.Effects of fluid-structure interaction on trailing-edge noise.J Mech Sci Technol,2008,22:1426-1435
    21刘占生,马瑞贤,杨帆,等.基于流固耦合作用的柔性体流噪声降噪机理研究.机械工程学报,2016,52:176-184
    1) 蒋树杰, 刘菲菲, 陈刚. 流固耦合振动效应对机翼气动噪声辐射的影响研究. 振动与冲击, 已接收

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