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A New Miniature Wind Turbine for Wind Tunnel Experiments. Part II: Wake Structure and Flow Dynamics

机译:一种用于风洞实验的新型微型风力发电机。第二部分:尾迹结构和流动动力学

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An optimized three-bladed horizontal-axis miniature wind turbine, called WiRE-01, with the rotor diameter of 15 cm is designed and fully characterized in Part I of this study. In the current part of the study, we investigate the interaction of the turbine with a turbulent boundary layer. The comparison of the spectral density of the thrust force and the one of the incoming velocity revealed new insights on the use of turbine characteristics to estimate incoming flow conditions. High-resolution stereoscopic particle image-velocimetry (S-PIV) measurements were also performed in the wake of the turbine operating at optimal conditions. Detailed information on the velocity and turbulence structure of the turbine wake is presented and discussed, which can serve as a complete dataset for the validation of numerical models. The PIV data are also used to better understand the underlying mechanisms leading to unsteady loads on a downstream turbine at different streamwise and spanwise positions. To achieve this goal, a new method is developed to quantify and compare the effect of both turbulence and mean shear on the moment of the incoming momentum flux for a hypothetical turbine placed downstream. The results show that moment fluctuations caused by turbulence are bigger under full-wake conditions, whereas those caused by mean shear are clearly dominant under partial-wake conditions. Especial emphasis is also placed on how the mean wake flow distribution is affected by wake meandering. Conditional averaging based on the instantaneous position of the wake center revealed that when the wake meanders laterally to one side, a high-speed region exists on the opposite side. The results show that, due to this high-speed region, large lateral meandering motions do not lead to the expansion of the mean wake cross-section in the lateral direction.
机译:设计了一种优化的三叶片水平轴微型风力涡轮机,称为WiRE-01,转子直径为15 cm,并在本研究的第一部分中进行了全面介绍。在当前的研究中,我们研究涡轮与湍流边界层的相互作用。推力的频谱密度与进入速度之一的频谱密度的比较揭示了使用涡轮机特性来估计进入流动条件的新见解。涡轮机在最佳条件下运行后,还执行了高分辨率立体粒子图像测速(S-PIV)测量。介绍并讨论了有关涡轮尾流速度和湍流结构的详细信息,这些信息可以用作验证数值模型的完整数据集。 PIV数据还用于更好地理解导致下游涡轮机在不同的流向和跨度位置处产生不稳定载荷的潜在机理。为了实现这个目标,开发了一种新方法来量化和比较湍流和平均剪切对放置在下游的假设涡轮机的传入动量通量矩的影响。结果表明,在全苏醒条件下,湍流引起的力矩波动较大,而在部分苏醒条件下,由平均剪切引起的力矩波动明显占主导。还特别强调了尾流蜿蜒如何影响平均尾流分布。基于尾流中心的瞬时位置的条件平均显示,当尾流从侧面向一侧蜿蜒曲折时,在另一侧存在一个高速区域。结果表明,由于该高速区域,大的横向曲折运动不会导致平均尾流横截面在横向方向上的扩展。

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