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微型扑翼飞行器空气动力学研究进展 被引量:7

Advances in Aerodynamics Research on Flapping-Wing Micro Air Vehicles
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摘要 微型扑翼飞行器(FMAV)作为一种新概念的航空器,有着广泛的功能和用途,已经受到了各国的高度重视.综述了国内外对微型扑翼飞行器的低雷诺数空气动力学问题的研究现状及未来的发展趋势,讨论了目前研究中需要解决的一些关键技术.在此基础上,总结出今后研究的重点,并为微型扑翼飞行器的设计提供了参考依据. Flapping-Wing Micro Air Vehicle (FMAV), as a new conceptual vehicle, provides a variety of functions and uses and has attracted much research attention in industrial nations. The present research situation and future development trend of the low Reynolds number aerodynamics of flapping-wing micro air vehicle (FMAV) are surveyed and several key technologies of FMAV are discussed. On this basis, the emphasis of future work of FMAV is summarized and the reference data for future design of FMAV is orovided in the end.
出处 《华东交通大学学报》 2007年第1期57-59,84,共4页 Journal of East China Jiaotong University
关键词 微型扑翼飞行器 气动特性 低雷诺数 非定常流动 flapping-wing micro air vehicle (FMAV) aerodynamic characteristics vlow Reynolds number non-steady flow
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参考文献25

  • 1Weis-Fogh and M.Jensen,Proc.R.Soc.London B,239,415(1956).
  • 2G.R.Spedding,Contemp.Math,141,401(1993).
  • 3R.Dudley,The Biomechanics of Insect Flight,Priceton University Press,Princeton,2000.
  • 4C.P.EllingTon,Philos.Trans.R.Soc.London B,305,1(1984).
  • 5孙茂.昆虫飞行的高升力机理[J].力学进展,2002,32(3):425-434. 被引量:43
  • 6Ellington C P,Van den Berg C,Willmott A P,et al.Leading Edge Vortices in Insect Flight[J].Nature,1996,384:626~630.
  • 7Van den Birg C,Ellington C P.The three-dimensional leading-edge vortex of a 'hovering' model howkmoth[J].Phil Trans R SocLond B,1997,352:329~340.
  • 8Liu H,Ellington C P,Kawachi K,et al.A computational fluid dynamic study of hawkmoth hovering[J].J Exp Biol,1998,201:461~477.
  • 9Wang Z J.Vortex shedding and frequency selection in flapping flight[J].J Fluid Mech,2000a,410:323~341.
  • 10Lan S L,Sun M.Aerodynamic properties of a wing performing unsteady rotational motions at low Reynolds number[J].Acta Mech,2001,149:135~147.

二级参考文献25

  • 1余永亮,童秉纲,马晖扬.AN ANALYTIC APPROACH TO THEORETICAL MODELING OF HIGHLY UNSTEADY VISCOUS FLOW EXCITED BY WING FLAPPING IN SMALL INSECTS[J].Acta Mechanica Sinica,2003,19(6):508-516. 被引量:20
  • 2刘岚,方宗德,侯宇,傅卫平,吴立言.微型扑翼飞行器的气动建模分析与试验[J].航空动力学报,2005,20(1):22-28. 被引量:15
  • 3赵攀峰,刘春阳,魏榛,李振国,刘曦,郑明章,杨基明.一种扑翼运动的模型实验及流场测量方法[J].实验力学,2004,19(4):408-414. 被引量:6
  • 4[1]Katz J, Plotkin A. Low speed aerodynamics: From wing theory to panel methods[M].New York: McGraw-Hill Book Co,1991
  • 5[2]Giesing. Nonlinear two-dimension unsteady potential flow with lift[J]. Journal of Aircraft, 1968,5(2):135~143
  • 6[3]Basu, Hancock. The unsteady motion of a two-dimension aerofoil in incompressible inviscid flow[J]. Journal of Fluid Mechanics, 1978,87:159~178
  • 7[4]Hall K C, Pigott S A. Power requirements for large-amplitude flapping flight[R]. AIAA 97-0827,1997.6~9
  • 8[5]Attenborouch D. The mastery of flight[R]. BBC VCD, ISRC CN-A01-01-0010-0/V.G3
  • 9[6]Tobalske. Kinematics of flap-bounding flight in the zebra finch over a Widerange of Speeds[J]. The Journal of Experimental Biology, 1999.1725~1739
  • 10[7]McCroskey W J, McAlister K W, Carr L W,et al. Dynamic stall on advanced airfoil sections[J]. Journal of the American Helicoper Society, 1981,26(3):40~50

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二级引证文献16

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