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Laser Doppler Velocimetry (LDV) measurements of airfoil surface flow on a Horizontal Axis Wind Turbine in boundary layer

机译:激光多普勒测速(LDV)测量边界层中水平轴风力涡轮机上的机翼表面流

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This study investigated the flow characteristics of a Horizontal Axis Wind Turbine (HAWT) rotor surface during rotation with wind tunnel experiments. Firstly, the effect of Laser Doppler Velocimetry (LDV) system on the power coefficient of HAWT was measured. Then, the flow distributions near the blade surface were measured at the different radial positions (r/R = 0.3 and 0.7) in the cases of the low and optimal tip speed ratios. At last, the radial position effect on the flow field features in boundary layer were also investigated in detail. As a result, the boundary layer thickness decreased at the blade leading edge and then increased rapidly along the blade surface at the trailing edge region. Furthermore, in the case of r/R = 0.7, the two-dimensional resultant velocity in the acceleration region of boundary layer showed smaller value than that of r/R = 0.3. Meanwhile, the flow in the blade root showed a large expansion of the deceleration zone at the low tip speed ratio. The results acquired from this study was suitable for designing the airfoil and had a better understanding of the radial position effect on dynamic stall. (C) 2019 Elsevier Ltd. All rights reserved.
机译:本研究通过风洞实验研究了旋转过程中水平轴风力涡轮机(HAWT)转子表面的流动特性。首先,测量了激光多普勒测速(LDV)系统对HAWT功率系数的影响。然后,在低速和最佳叶尖速度比的情况下,在不同的径向位置(r / R = 0.3和0.7)处测量叶片表面附近的流量分布。最后,研究了径向位置对边界层流场特征的影响。结果,边界层厚度在叶片前缘处减小,然后在叶片后缘区域处沿着叶片表面迅速增加。此外,在r / R = 0.7的情况下,边界层的加速区域中的二维合成速度显示出小于r / R = 0.3的值。同时,在低叶尖速比下,叶根中的流动显示出减速区的大扩展。从这项研究中获得的结果适合于设计机翼,并更好地了解了径向位置对动态失速的影响。 (C)2019 Elsevier Ltd.保留所有权利。

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