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Analysis of Vertical Axis Wind Turbine Aerodynamics by Using a Multi-Fidelity Approach

机译:垂直轴风力机空气动力学的多保真度分析

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This paper compares several methods for predicting the vertical axis wind turbine's aerodynamic performance, loading patterns as well as wake system behind the turbine. Three distinct aerodynamic prediction methodologies are implemented and compared with each other. One method is a low complexity analysis that improves the double-multiple streamtube model which is based on the traditional Blade Element Momentum theory. Another method is a medium complexity analysis which utilizes a potential flow model based on the calculation of the velocity field through the influence of the near wake system by applying the the three-dimensional panel method to the rotorl whole blade analysis. The last method is a high complexity analysis that utilizes the overset grid based full computational fluid dynamics method, in which each blade of the turbine will be modeled by using body conforming structured curvilinear meshes. Two different test cases are studied in order to highlight and characterize the prediction capabilities of all the approaches. The computational results of the aerodynamic loads acting on the rotor blades and whole turbine's power coefficient, which are obtained by three approaches, will be compared with the experimental data. Furthermore, the wind deficits generated by an isolated turbine are investigated by utilizing the subset of methodologies that allow for probing of flow field information such as velocity magnitude contours and wake trajectory behind the turbine. Finally, the advantage and disadvantage of each method are discussed so that the appropriate model can be applied to solve the desired engineering cases in more efficient ways.
机译:本文比较了几种用于预测垂直轴风力涡轮机的空气动力性能,载荷模式以及涡轮机背后的尾流系统的方法。实施了三种不同的空气动力学预测方法,并进行了相互比较。一种方法是低复杂度分析,它改进了基于传统叶片元素动量理论的双倍流管模型。另一种方法是中等复杂度分析,该方法通过将三维面板法应用于旋翼全叶片分析,利用基于近场系统影响的速度场计算得出的势流模型。最后一种方法是高复杂度分析,该分析利用基于过度网格的完整计算流体动力学方法,其中将通过使用符合人体的结构化曲线网格来对涡轮机的每个叶片进行建模。为了突出并表征所有方法的预测能力,研究了两个不同的测试用例。通过三种方法获得的作用在转子叶片上的空气动力载荷和整个涡轮机的功率系数的计算结果将与实验数据进行比较。此外,通过利用方法的子集来研究由隔离式涡轮机产生的风力不足,该方法学子集允许探测流场信息,例如速度大小轮廓和涡轮机后的尾流轨迹。最后,讨论了每种方法的优缺点,以便可以使用适当的模型以更有效的方式解决所需的工程案例。

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