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Lift enhancement of airfoil and tip flow control for wind turbine
  • ISSN号:0253-4827
  • 期刊名称:《应用数学和力学:英文版》
  • 时间:0
  • 分类:O354.1[理学—流体力学;理学—力学]
  • 作者机构:[1]Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P. R. China
  • 相关基金:Project supported by the National Basic Research Program of China (973 Program) (No. 2007CB714600)
中文摘要:

Two techniques that improve the aerodynamic performance of wind turbine airfoils are described.The airfoil S809,designed specially for wind turbine blades,and the airfoil FX60-100,having a higher lift-drag ratio,are selected to verify the flow control techniques.The flow deflector,fixed at the leading edge,is employed to control the boundary layer separation on the airfoil at a high angle of attack.The multi-island genetic algorithm is used to optimize the parameters of the flow deflector.The results indicate that the flow deflector can suppress the flow separation,delay the stall,and enhance the lift.The characteristics of the blade tip vortex,the wake vortex,and the surface pressure distributions of the blades are analyzed.The vortex diffuser,set up at the blade tip,is 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 the blade tip vortex,lower the noise,and improve the efficiency of the blade.

英文摘要:

Two techniques that improve the aerodynamic performance of wind turbine airfoils are described. The airfoil $809, designed specially for wind turbine blades, and the airfoil FX60-100, having a higher lift-drag ratio, are selected to verify the flow control techniques. The flow deflector, fixed at the leading edge, is employed to control the boundary layer separation on the airfoil at a high angle of attack. The multi-island genetic algorithm is used to optimize the parameters of the flow deflector. The results indicate that the flow deflector can suppress the flow separation, delay the stall, and enhance the lift. The characteristics of the blade tip vortex, the wake vortex, and the surface pressure distributions of the blades are analyzed. The vortex diffuser, set up at the blade tip, is 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 the blade tip vortex, lower the noise, and improve the efficiency of the blade.

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期刊信息
  • 《应用数学和力学:英文版》
  • 主管单位:交通部
  • 主办单位:上海大学
  • 主编:周哲玮
  • 地址:上海市宝山区上大路99号上海大学122信箱
  • 邮编:200444
  • 邮箱:amm@department.shu.edu.cn
  • 电话:021-66135219 66165601
  • 国际标准刊号:ISSN:0253-4827
  • 国内统一刊号:ISSN:31-1650/O1
  • 邮发代号:
  • 获奖情况:
  • 上海市优秀科技期刊一等奖,中国期刊方阵“双效”期刊
  • 国内外数据库收录:
  • 美国数学评论(网络版),波兰哥白尼索引,德国数学文摘,荷兰文摘与引文数据库,美国工程索引,美国科学引文索引(扩展库),英国科学文摘数据库,日本日本科学技术振兴机构数据库,美国应用力学评论
  • 被引量:541