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Performance improvement of a vertical axis wind turbine by comprehensive assessment of an airfoil family

机译:通过对翼型系列进行综合评估来改善垂直轴风力发电机的性能

摘要

Studies on lift-type VAWTs are far fewer than those on horizontal VAWTS, especially in the field of airfoil, which is regarded as the fundamental of VAWT design. Existing researches seldom systematically and efficiently touch upon a specific airfoil family. Thus, a coupled approach comprising two steps was used in this paper to assess an airfoil family, wherein the first step was the orthogonal algorithm combined with an automatic computational fluid dynamic analysis (ACFDA) module, and the second step was the combination of the one-factor at a time (OFAAT) algorithm and the ACFDA module. Results demonstrate that among three design parameters, the thickness-chord ratio (TCR) had the biggest effect on CP while the maximum thickness in tenths of chord (MTITOC) had the smallest influence on CP. By this approach, we found a desired airfoil having maximum power coefficient(CPMAX) was 0.4585, app. 15.5% higher than that of the previously widely used rotor NACA 0015. In addition, detailed flow data (field) dispersing in the vicinity of the airfoil were visualized to reveal the effect of each design parameter on airfoil's aerodynamic behavior. Lastly, this coupled approach can be used to assess any airfoil family that can be parameterized and has several design parameters.
机译:升力型VAWT的研究远远少于水平VAWTS,尤其是在机翼领域,这被认为是VAWT设计的基础。现有研究很少系统地和有效地涉及特定的机翼家族。因此,本文采用包括两个步骤的耦合方法来评估机翼系列,其中第一步是将正交算法与自动计算流体动力学分析(ACFDA)模块结合使用,而第二步是将两者结合使用一次因子(OFAAT)算法和ACFDA模块。结果表明,在三个设计参数中,厚度弦比(TCR)对CP的影响最大,而十分之一弦的最大厚度(MTITOC)对CP的影响最小。通过这种方法,我们发现具有最大功率系数(CPMAX)为0.4585的所需翼型,app。比以前广泛使用的转子NACA 0015高出15.5%。此外,可视化了散布在翼型附近的详细流动数据(场),以揭示每个设计参数对翼型空气动力性能的影响。最后,这种耦合方法可用于评估可以参数化并具有多个设计参数的任何机翼系列。

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