期刊文献+

最优S型小翼影响近尾迹流动的PIV测试 被引量:1

PIV Experiment on the Effect of Near Wake Using Horizontal Axis Wind Turbine With Optimal Ogee Tip Vane
原文传递
导出
摘要 在水平轴风力机叶尖添加结构合适的小翼,可以改变风轮表面的压力分布,提高功率输出,并调整风轮的动频曲线走势,改善其结构动态特性。本文提出S型叶尖小翼结构形式,采用5因素5水平的正交实验方法,找到在不同尖速比下均具有较好功率放大效果的最优叶尖小翼结构。采用轴编码器定位周期采样技术,在直流式低速风洞开口段对动态旋转风力机添加最优S型小翼和不添加小翼时的近尾迹流动进行了对比PIV测试。结果表明,结构合适的S型叶尖小翼可以打散从风轮叶尖脱落的叶尖涡结构,在测试方位面内形成多个涡量集中区域,而且使叶尖涡内高涡量区域减小,降低叶尖涡的强度,改善风轮的空气动力学特性,提高风轮的功率系数。 The horizontal axis wind turbine with the structure appropriate tip vane can change the pressure distribution of blade surface, improve power output, adjust the rotor dynamic frequency curve, and improve the structural dynamic characteristics of rotor. This paper elaborates the design of the ogee tip vane. The tip vane with preferable power augmentation effect was found by L25 experiment. The PIV measure of near wake dynamic flow of the rotating wind turbine with ogee tip vane and without tip vane was carried out using axis-coder phase-locked periodic sampling technology at wind tunnel opening. The experimental results show that the tip vane can diffuse and weaken the tip vortex, therefore, can improve aerodynamic characteristics and power coefficient of rotor.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2011年第12期2044-2047,共4页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.50976047) 内蒙古自治区高等学校科学研究项目(No.NJ10080)
关键词 水平轴风力机 尾迹 叶尖小翼 涡量 horizontal axis wind turbine wakel tip vane vorticity
  • 相关文献

参考文献5

二级参考文献19

  • 1汪建文,贾瑞博,吴克启,王军.小翼对风力机叶片表面压力分布的影响[J].工程热物理学报,2006,27(5):760-762. 被引量:25
  • 2Ebert P R, Wood D H. The Near Wake of a Model Horizontal-Axis Wind Turbine, Part 3: Properties of the Tip and Hub Vortices [J]. Renewable Energy, 2001, 22(1): 461-472.
  • 3Wood D H. Generic Vortex Modelling for Horizontal-Axis Wind Turbines [J]. Wind Engineering, 2002, 26(2): 71-84.
  • 4Leishman J G, Bhagwat M, Bagai A. Free-Vortex Filament Methods for the Analysis of Helicopter Rotor Wakes [J]. J. Aircraft, 2002, 39(5): 759-775.
  • 5Wagner S, Bareis R, Guidati G. Wind Turbine Noise [M]. Berlin: Springer, 1996:172-177.
  • 6Adrain R J. Twenty Years of Particle hnage Velocimetry [J]. Experiments in Fluids, 2005, 39(2): 159-169.
  • 7Van Holten.Windmill with Diffuser Effect Induced by Small Tip Vanes.In:Proc.Inst.System.Wind Energy Syst..Camdridge,U.K.,1976
  • 8Van Bussel G J W.Status Rep.on Tip Vane Research.In:Proc.Inst.EWEA Conference.Rome,1986.691-695
  • 9Shimizu Y,Yoshikawa T,Mastumura S.Power Augmentation Effects of a Horizontal Axis Wind Turbine with a Tip Vane-Part1:Turbine Performance and Tip Vane Configuration.Trans.ASME,J.Fluids Eng.,1994,116(6):287-292
  • 10Shimizu Y,Imamura H,Matsumura S,et al.Effects of Mie Tip Vane on Pressure Distribution of Rotor Blade and Power Augmentation of Horizontal Axis Wind Turbine.In:Proc.Int.ISROMAC-8.Hawaii,2000.42-48

共引文献54

同被引文献15

  • 1艾德·奥波特.运输类飞机的空气动力设计[M].顾诵芬,吴兴世,杨新军,译.上海:上海交通大学出版社,2010:240-303.
  • 2Richard S Shevell, Roger D Schaufele. Aerodynamic design {eaturesof the DC-9[J]. Journal o{ Aircraft, 1966, 3(6): 515-523.
  • 3杨士普,孙一峰,方阳.民机迎角传感器布局流场分析[c]∥昆明:第九届全国流动显示学术会议论文集,2012.
  • 4Wimpress J K. Predicting the low-speed stall characteristics of the Boeing 747[C]. AGARE>CP 102, 1972.
  • 5Ccpany D A. Aerodynamics of high-lit't airfoil systems[J]. Fluid Dynamics of Aircraft Stalling, 1972.
  • 6Gratzer L B. Analysis of transport applications for high-lift schemes[C]. AGARDLS43, 1970.
  • 7Burr D O' Laughlin, Lloyd Graham E, John Christiansen. S 3A development tests[C]. AIAA-73-778, 1973.
  • 8Hiroyuki Kato, Shigeya Watanabe, Mitsuhiro Murayama, et al. PIV investigation of nacelle Chine effects on high-lift system performance[C]. AIAA 2008 240, 2008.
  • 9袁红刚,李进学,杨永东,王天虹.前飞状态旋翼尾迹测量试验研究[J].实验流体力学,2010,24(4):29-32. 被引量:5
  • 10叶军科,陈迎春,李亚林,宋笔锋.民用飞机前缘增升装置气动特性试验研究[J].西北工业大学学报,2011,29(6):904-908. 被引量:3

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部