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首页> 外文期刊>International journal of green energy >An optimized airfoil geometry for vertical-axis wind turbine applications
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An optimized airfoil geometry for vertical-axis wind turbine applications

机译:针对垂直轴风力涡轮机应用的优化翼型几何形状

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摘要

In this work, a new airfoil shape optimized for vertical-axis wind turbine applications is proposed. Different airfoil shapes have been analyzed with JavaFoil, a panel method software. Then, the results from the analysis have been used to optimize the performance of the new airfoil shape. Afterward, Computational Fluid Dynamics (CFD) simulations of the proposed airfoil, UO-17-LDA, are run for different angles of attack to provide insight into the flow field and the mechanisms related to this increase in performance. The UO-17-LDA airfoil presents a high lift-to-drag ratio and a delayed stall angle with respect to the original FX-63-137 airfoil, making it suitable for vertical-axis wind turbine applications. This increase in performance has been verified by comparing two VAWT designs with the original and the proposed airfoil using a double-multiple streamtube model. Finally, the practicality of JavaFoil for the comparison of different airfoil geometries has been verified, as it is capable of obtaining results for a wide number of flow conditions in small computational times and with a user-friendly interface. Nevertheless, the results diverge from the actual solution for high angles of attack (beyond stall). Hence, the time and effort required to perform CFD simulations is justified to gain insight into the actual behavior of a particular airfoil, as well as to obtain a richer analysis of the flow field and the mechanisms related to the airfoil performance.
机译:在这项工作中,提出了一种针对垂直轴风力涡轮机应用进行了优化的新型翼型。已使用面板方法软件JavaFoil分析了不同的机翼形状。然后,分析的结果已用于优化新翼型形状的性能。然后,针对不同的迎角对拟议的机翼UO-17-LDA进行计算流体动力学(CFD)仿真,以深入了解流场以及与此性能提高相关的机制。与原始FX-63-137机翼相比,UO-17-LDA机翼具有较高的升阻比和延迟的失速角,使其适用于垂直轴风力涡轮机应用。通过使用双倍流管模型将两种VAWT设计与原始翼型和提议的翼型进行比较,已验证了这种性能提升。最终,JavaFoil用于比较不同的机翼几何形状的实用性已得到验证,因为它能够以较小的计算时间并通过用户友好的界面获得多种流动条件的结果。但是,结果与高攻角(超出失速)的实际解决方案有所不同。因此,进行CFD仿真所需的时间和精力是合理的,以便深入了解特定翼型的实际行为,并获得对流场和与翼型性能相关的机理的更丰富的分析。

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