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Experimental and Computational Investigation of a Small-Scale Vertical Axis Wind Turbine with Dynamic Blade Pitching

机译:动态叶片俯仰的小型垂直轴风力发电机的实验与计算研究

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This paper describes the systematic performance measurements and computational (CFD) studies conducted to investigate the performance of a small-scale dynamic-pitch vertical axis wind turbine (VAWT). The VAWT prototype was built and tested in a wind tunnel to understand the role of blade-pitch kinematics and flow curvature effects on turbine aerodynamic efficiency. The three parameters investigated in the experimental study were blade pitching amplitude (symmetric pitching), asymmetry in pitch kinematics between frontal and rear halves, and blade chord (or chord/radius ratio). Even though the optimal pitch amplitude is dependent on the tip speed ratio (TSR), moderate pitch amplitudes (± 20) had the highest overall efficiency for the symmetric pitch cases. The tip speed ratio corresponding to the maximum C_p decreased with increasing pitch amplitudes. The TSR corresponding to maximum Cp for 20° pitch amplitude was around 1.4, while the optimal TSR for the 40° case was around 0.7. Because of the differences in the flow velocities in the front and rear halves, for maximizing power extraction, the pitch angles required in the front is significantly higher than that in the rear. The optimal performance of the turbine occurred at a phasing of 0°. However, the performance was observed to be forgiving for small changes in phasing (<10°) in the positive direction (phase-lead), however, not in the negative direction. Increasing the chord/radius from 0.19 to 0.25 caused significant improvements in turbine efficiency especially at higher pitch amplitudes because of the flow curvature effects. A CFD model was developed and extensively validated with the present experimental data. The validated CFD model was used to understand the effect of the different parameters on turbine performance by analyzing the blade aerodynamics at various azimuthal locations. CFD analysis showed that the blade extracts most of the power in the frontal half of its circular trajectory and in some cases even lose power in the rear half. This study clearly indicates the potential for major improvements in VAWT performance with novel blade kinematics, optimal chord/radius ratio, and using cambered blades.
机译:本文介绍了系统性能测量和计算(CFD)研究,旨在研究小型动态螺距垂直轴风力涡轮机(VAWT)的性能。 VAWT原型是在风洞中建造和测试的,以了解叶片桨距运动学和流曲率对涡轮空气动力效率的作用。在实验研究中研究的三个参数是桨距变化幅度(对称桨距),前半部和后半部之间的桨距运动学上的不对称性以及桨叶弦(或弦/半径比)。即使最佳音高幅度取决于尖端速度比(TSR),对于对称音高情况,中等音高幅度(±20)仍具有最高的整体效率。对应于最大C_p的叶尖速度比随着螺距幅度的增加而降低。对应于20°俯仰幅度的最大Cp的TSR约为1.4,而40°情况下的最佳TSR约为0.7。由于前半部和后半部的流速不同,为了最大程度地提取功率,前部所需的俯仰角明显高于后部。涡轮的最佳性能出现在相位为0°的位置。但是,观察到在正方向(相位超前)的相位变化(<10°)很小,但在负方向上的变化很小,这是可以接受的。将弦/半径从0.19增加到0.25会导致涡轮效率的显着提高,尤其是在较高的螺距振幅下,由于流动曲率效应,涡轮效率会大大提高。开发了CFD模型,并使用当前的实验数据进行了广泛的验证。经过验证的CFD模型用于通过分析各个方位角位置的叶片空气动力学来了解不同参数对涡轮性能的影响。 CFD分析表明,叶片在圆形轨迹的前半部提取了大部分动力,在某些情况下甚至在后半部损失了动力。这项研究清楚地表明,通过新颖的叶片运动学,最佳弦/半径比以及使用弧形叶片,可以显着改善VAWT性能。

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