首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >Aerodynamic performance enhancement analysis of horizontal axis wind turbines using a passive flow control method via split blade
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Aerodynamic performance enhancement analysis of horizontal axis wind turbines using a passive flow control method via split blade

机译:水平轴风风力涡轮机通过分流刀片使用无源流量控制方法的空气动力学性能增强分析

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摘要

Horizontal axis wind turbines (HAWTs) are being widely used for green energy generation. Hence, aerodynamic performance enhancement of these machines is a key point for their overall performances. This paper numerically investigates effects of a passive flow control method on aerodynamic performance of a HAWT by splitting its blades along the span. First, 2-D simulations are conducted on 5809 airfoil in order to study effects of split width and Reynolds. Later, original blade (without split) and two split blades are simulated, and effects of split location on power coefficient, low speed shaft torque and flow patterns are investigated at different tip speed ratios. The results reveal that for an attached flow, torque value are sensitively dependent upon split location and injected flow angle. This is because injected flow triggers an early separation and reduces aerodynamic performance. For a partially separated case, results show that split location may impose either positive or negative effects on torque generation. Finally, for highly separated/stall situations, blade aerodynamic performance becomes less sensitive to the location of split. Also, torque per unit span analysis shows that as tip speed ratio decreases the split part of the blade generates a higher share of the total power.
机译:水平轴风力涡轮机(HAWTS)广泛用于绿色能源。因此,这些机器的空气动力学性能增强是整体性能的关键点。本文通过沿跨度分裂其叶片来数值研究了被动流量控制方法对HAWT气动性能的影响。首先,在5809个翼型上进行2-D模拟,以研究分裂宽度和雷诺的影响。稍后,模拟原始刀片(没有分裂)和两个分割刀片,并以不同的尖端速度比对电力系数,低速轴扭矩和流动图案进行了分离位置的影响。结果表明,对于连接的流动,扭矩值敏感地依赖于分裂位置和喷射的流动角度。这是因为注入的流动触发早期分离并降低空气动力学性能。对于部分分离的情况,结果表明分裂位置可能对扭矩产生施加正面或负面影响。最后,对于高度分离的/失速情况,刀片空气动力学性能对分裂的位置变得不太敏感。此外,每单位跨度分析的扭矩表明,由于尖端速比降低了刀片的分开部分产生总功率的更高份额。

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