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风力机叶型增升及叶尖流动控制研究 被引量:2

Lift Enhancement of the Airfoil and Tip Flow Control for Wind Turbine
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摘要 研究了两种改善风力机叶型气动性能的流动控制技术,分别对风力机专用S809翼型和较大升阻比的FX 60-100翼型进行应用研究.首先,通过在叶型前缘加装流动偏转器,研究流动偏转器对叶型流动分离的控制效果.并采用多岛基因算法,对流动偏转器进行多参数优化.结果表明:流动偏转器可以有效控制叶型的失速特性,推迟失速攻角和增加升力;基因优化算法能更大地提升流动偏转器的控制效果.其次,基于对风力机叶尖旋涡和尾涡特征以及叶片表面压力分布的分析,在叶片尖部加装不同倾斜角的旋涡扩散器控制叶尖涡.结果表明:涡扩散器能够提高叶尖涡涡核的总压,削弱其旋涡强度,使风力机尾流旋涡耗散更快,从而可以减小噪声,提高叶片效率. Two techniques that improve the aerodynamic performance of wind turbine airfoils were described.The airfoil S809,often used for wind turbine design,and the airfoil FX 60-100,having higher lift-drag ratio,were selected to verify the flow control techniques.The flow deflector,fixed at the leading edge,was employed to control the boundary layer separation on the airfoil at high angle of attack.The multi-island genetic algorithm was used to optimize the parameters of the flow deflector.The results indicate that the flow deflector can suppress the flow separation,delay stall and enhance the lift.In the second part of this paper,the characteristics of the blade tip vortex,wake vortex and the surface pressure distributions of blades are analyzed.The vortex diffuser,set up at the blade tip,was employed to control the blade tip vortex.The results show that the vortex diffuser can increase the total pressure coefficient of the core of the vortex,decrease the strength of blade tip vortex,lower the noise and improve the efficiency of the blade.
出处 《应用数学和力学》 CSCD 北大核心 2011年第7期774-784,共11页 Applied Mathematics and Mechanics
基金 国家"973"基金资助项目(2007CB714600)
关键词 流动控制 流动分离 流动偏转器 多岛基因算法 叶尖涡 涡扩散器 flow control flow separation flow deflector multi-island genetic algorithm blade tip vortex vortex diffuser
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  • 1Grasso F. Usage of numerical optimization in wind turbine airfoil design[C]//28th AIAA Applied Aerodynamics Conference, 28-30 June 2010, 20104404. Chicago: USA AIAA.
  • 2Chang T L, Rachman A, Tsai H M. How control of an airfoil via injection and suction [ J ]. Journal of Aircraft, 2009, 46( 1 ) : 291-300.
  • 3Nikolic V R. Effect of gurney flap relative span on lift, drag, and trailing vortex of a rectangular wing[ C]//25th AIAA Applied Aerodynamics Conference, 25-28 June 2007, 2007-4062. Mianli: USA MAA.
  • 4李应红,吴云,张朴,苏长兵,宋慧敏.等离子体激励抑制翼型失速分离的实验研究[J].空气动力学学报,2008,26(3):372-377. 被引量:37
  • 5周立胜,明晓,白亚磊.流动偏转器对机翼失速特性的控制[J].空气动力学学报,2011,29(1):16-21. 被引量:4
  • 6Hansen Martin O L.风力机空气动力学[M].北京:中国电力出版社,2009.16-22.
  • 7Johasen J, Gaunaa M, Sorensen N. Increased aerodynamic efficiency on wind turbine rotor suing winglets[ C]//26th AIAA Applied Aerodynamics Conference, 18-21 August 2008, 2008- 6728. Hawaii: USA AIAA.
  • 8东雪青,汪建文,韩晓亮,高志鹰,刘冬冬,新吉勒图,仇连君.风力机叶尖加小翼流场的试验研究[J].工程热物理学报,2009,30(10):1662-1664. 被引量:8
  • 9余永生,杜向东,魏庆鼎.翼梢涡的结构与控制方法探索[J].空气动力学学报,1999,17(4):405-412. 被引量:8
  • 10MING Xiao. Drag reduction of a civil aircraft by wing tip devices[ C ]//Sixth Asian Conference of l-uid Mechanics. Singapore, 1995.

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