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BLADE DESIGN CRITERIA TO COMPENSATE THE FLOW CURVATURE EFFECTS IN H-DARRIEUS WIND TURBINES

机译:叶片设计准则,以补偿H-DARRIEUS风轮机中的流动弯曲效应

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Darrieus wind turbines are experiencing a renewed interest in the wind energy scenario, in particular whenever small and medium-size installations are considered. In these contexts, the average wind speeds are generally quite low due to scale effects and therefore the most exploited design choices for the turbines are the H-shape configuration, as the entire blade can take advantage of the maximum rotational radius, and high chord to radius ratios, in order to ensure suitable Reynolds numbers on the airfoils. By doing so, the aerodynamic effects induced by the motion of the airfoils in a curved flowpath become more evident and the airfoils themselves have to be designed to compensate these phenomena if conventional design tools based on the BEM theory are used. In this study, fully unsteady 2D simulations were exploited to analyze a three-bladed H-Darrieus wind turbine in order to define the real flow structure and its effects on the turbine performance; in detail, the influence of both the virtual camber and the virtual incidence were investigated. CFD results were supported by experimental data collected on full-scale models reproducing two different airfoil mountings. Finally, the proper design criteria to compensate these phenomena are proposed and their benefits on a conventional simulation with a BEM approach are discussed.
机译:达里厄斯(Darrieus)风力涡轮机在风能场景中正重新引起人们的兴趣,尤其是在考虑中小型安装时。在这些情况下,由于比例效应,平均风速通常会非常低,因此,涡轮机最受开发利用的设计选择是H形配置,因为整个叶片都可以利用最大旋转半径,并且弦长高。半径比,以确保翼型上具有合适的雷诺数。通过这样做,由翼型件在弯曲的流路中的运动引起的空气动力效应变得更加明显,并且如果使用基于BEM理论的常规设计工具,则必须设计型翼件自身以补偿这些现象。在这项研究中,利用完全不稳定的2D模拟来分析三叶片H-Darrieus风力涡轮机,以定义实际的流动结构及其对涡轮机性能的影响。详细地,研究了虚拟外倾角和虚拟入射角的影响。 CFD结果得到了在复制两个不同翼型支架的全尺寸模型上收集的实验数据的支持。最后,提出了补偿这些现象的适当设计准则,并讨论了它们在采用BEM方法进行的常规仿真中的好处。

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