Lift enhancement of airfoil and tip flow control for wind turbine

被引:12
作者
Bai, Ya-lei [1 ]
Ma, Xing-yu [1 ]
Ming, Xiao [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Dept Aerodynam, Nanjing 210016, Peoples R China
关键词
flow separation; flow control; flow deflector; multi-island genetic algorithm; tip vortex diffuser;
D O I
10.1007/s10483-011-1462-8
中图分类号
O29 [应用数学];
学科分类号
070104 ;
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.
引用
收藏
页码:825 / 836
页数:12
相关论文
共 14 条
[1]   COMPARISON OF WIND-TUNNEL AIRFOIL PERFORMANCE DATA WITH WIND TURBINE BLADE DATA [J].
BUTTERFIELD, CP ;
SCOTT, G ;
MUSIAL, W .
JOURNAL OF SOLAR ENERGY ENGINEERING-TRANSACTIONS OF THE ASME, 1992, 114 (02) :119-124
[2]   Flow Control of an Airfoil via Injection and Suction [J].
Chng, T. L. ;
Rachman, A. ;
Tsai, H. M. ;
Zha, Ge-Cheng .
JOURNAL OF AIRCRAFT, 2009, 46 (01) :291-300
[3]  
DONG XQ, 2009, J ENG THERMOPHYSICS, V30, P1162
[4]  
GRASSO F, 2010, 28 AIAA APPL AER C C
[5]  
Han Z., 2004, The FLUENT fluid project simulates calculating an example and applies
[6]  
Hansen M.O.L., 2009, AERODYNAMICS WIND TU
[7]   Optimization of airfoil flow control using a genetic algorithm with diversity control [J].
Huang, Liang ;
Huang, George ;
LeBeau, Raymond .
JOURNAL OF AIRCRAFT, 2007, 44 (04) :1337-1349
[8]  
Johasen J., 2008, 26 AIAA APPL AER C H, P2008
[9]  
[李应红 LI Yinghongv], 2008, [空气动力学学报, Acta Aerodynamica Sinica], V26, P372
[10]  
MING X, 1995, 6 AS C FLUID MECH SI