Effect of protuberances on the aerodynamic performance of a wind turbine blade - a review

被引:0
|
作者
Maurya, Nancy [1 ]
Patil, Anuj U. [1 ]
Salunkhe, Pramod B. [1 ]
Varpe, Mahesh [2 ]
机构
[1] Manipal Acad Higher Educ, Manipal Inst Technol, Dept Aeronaut & Automobile Engn, Manipal 576104, Karnataka, India
[2] MS Ramaiah Univ Appl Sci, Dept Aerosp Engn, Bengaluru, Karnataka, India
关键词
Leading edge protuberances; tubercles; power coefficient; wind turbine performance; horizontal axis wind-turbine; vertical axis wind-turbine; LEADING-EDGE TUBERCLES; HUMPBACK WHALE; TRAILING-EDGE; VERTICAL-AXIS; AIRFOIL; FLOW; STALL; AEROFOIL; DESIGN; REDUCTION;
D O I
10.1080/15567036.2024.2321294
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This paper thoroughly reviews the influence of protuberances on the performance of a wind-turbine blade in terms of aerodynamic characteristics, power generation capability, and noise emission. It is observed that the protuberances are significantly useful in improving the aerodynamic performance of wind turbine blades, especially in the post-stall regime and during fluctuating wind conditions, such as wind gusts. The protuberance amplitude was found to be the dominant parameter to influence the blade performance. The amplitude and wavelength were tested in the range of 2-12%c and 2-50%c, respectively. The highest wind turbine performance was observed at small amplitude and large wavelength in the pre-stall regime and at large amplitude and small wavelength in the post-stall regime. Incorporating leading edge protuberances may increase lift and power coefficients by 50 and 55%, respectively, and reduce noise emission by nearly 16 dB. With the increase in the angle of attack, the instability noise was found to change its form. The broadband noise forms at a lower angle of attack (similar to 2 degrees) which converts to the tonal noise at the angle of attack, 6.5 degrees. The protuberances substantially alter the boundary layer flow, subsequently modifying the pressure and velocity field over the suction surface of the blade. A pair of vortices forms across a protuberance, which exchanges momentum with the boundary layer flow and helps delay/eliminate the flow separation. This flow separation control is responsible for the benefits as mentioned above.
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页码:3416 / 3431
页数:16
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