Lanzhou University of Technology Institutional Repository (LUT_IR)
Analysis influence of trailing edge modification on aerodynamic performance of airfoils for wind turbine | |
Yuan, Shangke1,2; Li, Rennian2 | |
2012 | |
会议名称 | 2nd International Conference on Advanced Design and Manufacturing Engineering, ADME 2012 |
会议录名称 | Applied Mechanics and Materials |
卷号 | 220-223 |
页码 | 900-904 |
会议日期 | August 16, 2012 - August 18, 2012 |
会议地点 | Taiyuan, China |
出版者 | Trans Tech Publications, P.O. Box 1254, Clausthal-Zellerfeld, D-38670, Germany |
摘要 | The airfoil NACA 4412 commonly employed in wind turbines is modified by attaching a Gurney flap with length of 2% chord at its trailing edge and its remodeled form as well. The SIMPLE algorithm of finite volume method and software FLUENT are respectively used to carry out numerical computation of aerodynamic performances of above-mentioned three airfoils (including the un-modified one), so that their aerodynamic characteristics, pressure distribution on their surface, and streamline around them are obtained for different angles of attack. It is shown by the computation result that the modified airfoils will result in such a strong downwash effect that the pressure distribution on airfoil surface is remarkably altered, the lift coefficient and as well as the slope of lift-drag characteristic curve are increased, and meantime the airfoil stalling is greatly postponed. © (2012) Trans Tech Publications, Switzerland. |
关键词 | Design Finite volume method Lift Numerical methods Pressure distribution Wind turbines Aerodynamic characteristics Aerodynamic performance Airfoil surfaces Angles of attack Characteristic curve Gurney flaps Lift coefficient Numerical computations SIMPLE algorithm Software FLUENT Trailing edge modifications Trailing edges |
DOI | 10.4028/www.scientific.net/AMM.220-223.900 |
收录类别 | EI |
语种 | 英语 |
EI入藏号 | 20125015787799 |
EI主题词 | Airfoils |
ISSN | 16609336 |
来源库 | Compendex |
分类代码 | 408 Structural Design - 615.8 Wind Power (Before 1993, use code 611 ) - 651.1 Aerodynamics, General - 652.1 Aircraft, General - 921.6 Numerical Methods - 931.1 Mechanics |
引用统计 | |
文献类型 | 会议论文 |
条目标识符 | https://ir.lut.edu.cn/handle/2XXMBERH/116397 |
专题 | 兰州理工大学 能源与动力工程学院 新能源学院 |
作者单位 | 1.School of Energy and Power Engineering, Lanzhou University of Technology, Lanzhou 730050, China; 2.Architectural Engineering Department, Lanzhou Institute of Technology, Lanzhou 730050, China |
第一作者单位 | 新能源学院 |
推荐引用方式 GB/T 7714 | Yuan, Shangke,Li, Rennian. Analysis influence of trailing edge modification on aerodynamic performance of airfoils for wind turbine[C]:Trans Tech Publications, P.O. Box 1254, Clausthal-Zellerfeld, D-38670, Germany,2012:900-904. |
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