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首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >The role of free stream turbulence with large integral scale on the aerodynamic performance of an experimental low Reynolds number S809 wind turbine blade
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The role of free stream turbulence with large integral scale on the aerodynamic performance of an experimental low Reynolds number S809 wind turbine blade

机译:具有大整数比例的自由流湍流对实验性低雷诺数S809风力涡轮机叶片的空气动力学性能的作用

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Effects of free stream turbulence with large integral scale on the aerodynamic performance of an S809 airfoil-based wind turbine blade at low Reynolds number are studied using wind tunnel experiments. The case of wind turbine blades subjected to turbulence structures with large integral scale is of interest since in the atmospheric boundary layer very large-scale structures interact with the blades. A constant chord (2-D) S809 airfoil wind turbine blade model with an operating Reynolds number of 2.08 x 10(5) based on chord length was tested for a range of angles of attack representative of fully attached and stalled flow as encountered in typical wind turbine operation. The smooth-surface blade was subjected to a quasi-laminar free stream with very low free-stream turbulence as well as to elevated free-stream turbulence generated by an active grid. This turbulence contained large-scale eddies with levels of free-stream turbulence intensity of up to 6.14% and an integral length scale of about 60% of chord-length. The pressure distribution was acquired using static pressure taps and the lift was subsequently computed by numerical integration. The wake velocity deficit was measured utilizing hot-wire anemometry to compute the drag coefficient also via integration. In addition, the mean flow was quantified using 2-D particle image velocimetry (PIV) over the suction surface of the blade. Results indicate that turbulence, even with very large-scale eddies comparable in size to the chord-length, significantly improves the aerodynamic performance of the blade by increasing the lift coefficient and overall lift-to-drag ratio, LID for all angles tested except 0 degrees. Published by Elsevier Ltd.
机译:利用风洞实验研究了大积分自由流湍流对低雷诺数S809翼型风力发电机叶片空气动力性能的影响。风力涡轮机叶片经受具有大的整体尺度的湍流结构的情况是令人感兴趣的,因为在大气边界层中非常大的尺度的结构与叶片相互作用。测试了基于弦长的雷诺数为2.08 x 10(5)的恒定弦(2-D)S809翼型风力涡轮机叶片模型的迎角范围,代表了典型情况下遇到的完全附着和失速的流动风力发电机运行。使光滑表面的叶片经受具有非常低的自由流湍流的准层流自由流以及由有源栅格产生的升高的自由流湍流。这种湍流包含大型涡流,其自由流湍流强度水平高达6.14%,积分长度比例约为弦长的60%。使用静压抽头获取压力分布,然后通过数值积分计算升程。利用热线风速仪也通过积分计算了尾流速度的不足,以计算阻力系数。另外,使用叶片的吸力表面上的二维粒子图像测速(PIV)定量平均流量。结果表明,湍流,即使具有与弦长相当的非常大的涡流,也可以通过增加升力系数和总体升阻比(对于除0以外的所有角度)的LID来显着改善叶片的空气动力学性能。度。由Elsevier Ltd.发布

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