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

机译:具有动态刀片投球的小型垂直轴风力涡轮机的实验和计算研究

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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:本文介绍了进行的系统性能测量和计算(CFD)研究,以研究小型动态俯仰垂直轴风力涡轮机(VAWT)的性能。 VAWT原型在风洞中构建和测试,以了解刀片间动态的作用和对涡轮机空气动力学效率的流动曲率效应。在实验研究中研究的三个参数是叶片俯仰幅度(对称俯仰),正面和后半部之间的间距运动学中的不对称性,以及叶片弦(或弦/半径比)。尽管最佳音调幅度取决于尖端速比(TSR),所以适度间距幅度(±20)对于对称间距壳体具有最高的总体效率。对应于最大C_P的尖端速度比随着音高幅度的增加而降低。对应于20°音调幅度的最大CP的TSR约为1.4,而40°壳的最佳TSR约为0.7。由于前后半部的流速的差异,用于最大化功率提取,前面所需的俯仰角显着高于后部。涡轮机的最佳性能发生在0°的相位下。然而,观察到性能被宽加于正方向(相位引线)中的相位(<10°)的小变化,然而,不在负方向上。将弦/半径从0.19增加到0.25,由于流动曲率效应,尤其是在涡轮机效率的显着改善。通过本实验数据开发和广泛验证了CFD模型。通过分析各方位角位置的叶片空气动力学来使用验证的CFD模型来了解不同参数对涡轮机性能的影响。 CFD分析表明,刀片提取其圆形轨迹的正面半部的大部分电力,并且在某些情况下甚至在后半部分中失效。本研究清楚地表明了具有新型刀片运动学,最佳弦/半径比和使用弧形刀片的VAWT性能的主要改进的可能性。

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