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Numerical and experimental analysis of the twin-blade hydrofoil for hydro and wind turbine applications

机译:用于水轮机和风力涡轮机的双叶片水翼的数值和实验分析

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In this study, the hydrodynamic performance of a twin-blade hydrofoil has been numerically and experimentally investigated in three dimensions for tip speed ratios ranging between 1.5 and 5.5. The optimum geometric and flow parameters leading to the maximum value of the C-L/C-D ratio, which is the major design parameter of the wind and hydrokinetic turbines, have been determined. At a design flow velocity of 2 m/s (Re=3 x 10(5)) the maximum power coefficient of 0.457 was obtained at the tip velocity ratio of 3.5 at optimum geometric parameters of h/c(1) =0.667, c(1)/c(2)= 0.671 and the angle of attack of 3 degrees. The maximum torque of 224 Nm was obtained at the tip speed ratio of 2.5 for a prototype that has been built and tested during the experimental studies. The experimental studies were conducted in a towing tank, by which a power coefficient of 0.424 at the tip speed ratio of 3.48 was obtained. This speed ratio of 3.48 is about 7% lower than the numerical results. The optimum tip speed ratio of 3.5 is quite low when compared with the optimum tip speed ratio of 5.0 for the three bladed standard wind turbines. The advantage of employing twin-blade hydrofoils or airfoil is the potential of achieving better engineering designs and applications of wind and hydrokinetic turbines, which can be used for power generation purposes starting-up at lower wind and hydraulic current velocities. (C) 2015 Elsevier Ltd. All rights reserved.
机译:在这项研究中,双叶片水翼的水动力性能已在三个维度上进行了数值和实验研究,其叶尖速比范围为1.5至5.5。确定了导致C-L / C-D比最大值的最佳几何和流量参数,这是风力涡轮机和水动力涡轮机的主要设计参数。在设计流速为2 m / s(Re = 3 x 10(5))时,在最佳几何参数h / c(1)= 0.667,c时,尖端速度比为3.5时,最大功率系数为0.457。 (1)/ c(2)= 0.671,迎角为3度。对于在实验研究过程中制造和测试的原型,在尖端速度比为2.5时获得了224 Nm的最大扭矩。在拖曳罐中进行了实验研究,由此在3.48的叶尖速比下获得了0.424的功率系数。 3.48的速度比比数值结果低大约7%。与三叶片标准风力涡轮机的最佳尖端速度比5.0相比,其最佳尖端速度比3.5相当低。使用双叶片水翼或机翼的优势在于有可能实现风力涡轮机和水力涡轮机的更好的工程设计和应用,这些涡轮机可用于以较低风速和水力流速启动的发电目的。 (C)2015 Elsevier Ltd.保留所有权利。

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