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A case study on the calibration of the k-omega SST (shear stress transport) turbulence model for small scale wind turbines designed with cambered and symmetrical airfoils

机译:带有弧形和对称翼型的小型风力涡轮机的k-omega SST(剪切应力传递)湍流模型校准的案例研究

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This work presents a calibration study of the k-omega SST turbulence model for small scale wind turbines. To accomplish this, two different sets of blades were designed, built, tested and simulated. The first set applied the NACA 0012 and the second the NACA 4412 airfoil. The numerical investigation was taken using the CFD (computational fluid dynamics) code OpenFOAM and the turbulence model was calibrated testing several values for the beta*, including its canonical value, 0.09. The numerical calibration (the main contribution of this paper), extended previous results, which stated that different beta* values could calibrate the k-omega SST turbulence model for small wind turbines, mainly for the drag effects. The study broadened this conclusion, once the model was calibrated for a quite wide range of tip speed ratio values, from the turbine startup (lambda = 0) until its highest experimental value (lambda congruent to 8). As a secondary contribution, the results show that the model could be adjusted to simulate average field data, even though these being subject to its inherent variabilities. The main conclusion was that, for the sets of blades studied, the lowest RMSE value was obtained for beta* = 0.27. (C) 2015 Elsevier Ltd. All rights reserved.
机译:这项工作提出了用于小型风力涡轮机的k-omega SST湍流模型的校准研究。为此,设计,构建,测试和模拟了两组不同的刀片。第一套使用NACA 0012,第二套使用NACA 4412机翼。使用CFD(计算流体动力学)代码OpenFOAM进行了数值研究,并且对湍流模型进行了校准,以测试β*的多个值,包括其标准值0.09。数值校准(本文的主要贡献)扩展了先前的结果,该结果表明,不同的beta *值可以校准小型风力发电机的k-omega SST湍流模型,主要是针对风阻效应。一旦从涡轮机启动(lambda = 0)到最高试验值(lambda等于8)校正了范围广泛的叶尖速比值,研究便扩大了这一结论。作为次要贡献,结果表明,可以调整模型以模拟平均现场数据,即使这些数据受其固有的可变性影响。主要结论是,对于所研究的叶片组,对于β* = 0.27,获得了最低的RMSE值。 (C)2015 Elsevier Ltd.保留所有权利。

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