Studies on a low Reynolds number airfoil for small wind turbine applications

被引:18
|
作者
Wata, Joji [1 ]
Faizal, Mohammed [1 ]
Talu, Boniface [1 ]
Vanawalu, Lesia [1 ]
Sotia, Puamau [1 ]
Ahmed, M. Rafiuddin [1 ]
机构
[1] Univ S Pacific, Div Mech Engn, Suva, Fiji
关键词
low Reynolds number; airfoil; small wind turbines; pressure distribution; coefficient of lift; coefficient of drag; DESIGN; BEHAVIOR;
D O I
10.1007/s11431-011-4411-3
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In contrast to large horizontal axis wind turbines (HAWTs) that are located in areas dictated by optimum wind conditions, small wind turbines are required for producing power without necessarily the best wind conditions. A low Reynolds number airfoil was designed after testing a number of low Reynolds number airfoils and then making one of our own; it was tested for use in small HAWTs. Studies using XFOIL and wind tunnel experiments were performed on the new airfoil at various Reynolds numbers. The pressure distribution, C (p) , the lift and drag coefficients, C (L) and C (D) , were studied for varying angles of attack, alpha. It is found that the airfoil can achieve very good aerodynamic characteristics at different Reynolds numbers and can be used as an efficient airfoil in small HAWTs.
引用
收藏
页码:1684 / 1688
页数:5
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