首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Detailed Analysis of the Wake Structure of a Straight-Blade H-Darrieus Wind Turbine by Means of Wind Tunnel Experiments and Computational Fluid Dynamics Simulations
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Detailed Analysis of the Wake Structure of a Straight-Blade H-Darrieus Wind Turbine by Means of Wind Tunnel Experiments and Computational Fluid Dynamics Simulations

机译:直叶片H-Darrieus风力涡轮机尾流结构的风洞实验和计算流体动力学模拟的详细分析

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Darrieus vertical axis wind turbines (VAWTs) have been recently identified as the most promising solution for new types of applications, such as small-scale installations in complex terrains or offshore large floating platforms. To improve their efficiencies further and make them competitive with those of conventional horizontal axis wind turbines, a more in depth understanding of the physical phenomena that govern the aerodynamics past a rotating Darrieus turbine is needed. Within this context, computational fluid dynamics (CFD) can play a fundamental role, since it represents the only model able to provide a detailed and comprehensive representation of the flow. Due to the complexity of similar simulations, however, the possibility of having reliable and detailed experimental data to be used as validation test cases is pivotal to tune the numerical tools. In this study, a two-dimensional (2D) unsteady Reynolds-averaged Navier–Stokes (U-RANS) computational model was applied to analyze the wake characteristics on the midplane of a small-size H-shaped Darrieus VAWT. The turbine was tested in a large-scale, open-jet wind tunnel, including both performance and wake measurements. Thanks to the availability of such a unique set of experimental data, systematic comparisons between simulations and experiments were carried out for analyzing the structure of the wake and correlating the main macrostructures of the flow to the local aerodynamic features of the airfoils in cycloidal motion. In general, good agreement on the turbine performance estimation was constantly appreciated.
机译:Darrieus垂直轴风力涡轮机(VAWT)最近被公认为是新型应用的最有前途的解决方案,例如复杂地形中的小型安装或海上大型浮动平台。为了进一步提高其效率并使它们与传统的水平轴风力涡轮机竞争,需要更深入地了解通过旋转的Darrieus涡轮机控制空气动力学的物理现象。在这种情况下,计算流体动力学(CFD)可以发挥基本作用,因为它代表了唯一能够提供详细而全面的流动表示的模型。但是,由于类似模拟的复杂性,能否将可靠而详细的实验数据用作验证测试用例对于调整数值工具至关重要。在这项研究中,使用二维(2D)非稳态雷诺平均Navier-Stokes(U-RANS)计算模型来分析小型H形Darrieus VAWT的中平面尾迹特性。该涡轮机在大型开放式风洞中进行了测试,包括性能和尾流测量。由于可获得如此独特的一组实验数据,因此在模拟和实验之间进行了系统的比较,以分析尾流的结构并将旋流的主要宏观结构与摆线运动中的机翼的局部空气动力学特征相关联。总的来说,人们对涡轮性能评估的良好共识一直受到赞赏。

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