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Investigation of Near Wake Flow Structure of a Horizontal Axis Wind Turbine Using Particle Image Velocimetry

机译:基于粒子图像测速的水平轴风力发电机近尾流结构研究。

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摘要

An experimental study was conducted to investigate the mean and turbulent flow characteristics in the near wake region of a model horizontal axis wind turbine (HAWT), with the rotor diameter D = 0.15 m. State-of-the-art particle image velocimetry (PIV) technique was utilized to measure two dimensional velocity fields in horizontal planes, which extended between 0.15 D upstream to 0.7 D downstream. Measurements were taken at three vertical positions (z = 0.185 m, 0.135 m, and 0.05 m) to account for wake perturbations from the blades, support tower and blades, and the tower itself. The wind speed was varied to give a tip speed ratio (λ) range of 3.5 - 4.25 and chord Reynolds number between 1900 - 2500. udA phase averaging algorithm was developed according to the rotor’s angular configuration to compute various phase-averaged flow quantities. Results are presented in ensemble-averaged and phase-averaged forms. Results of phase averaged velocity deficit determined regions of accelerated flow adjacent to individual blades, and a localized region of lower momentum due to flow separation. The correlation between blade-trailing vorticity strength, and the increase in turbulence was confirmed through profiles of turbulence intensity. The profiles of Reynolds stress showed significant enhancement immediately downstream of blades and tower indicating the enhanced production of turbulent kinetic energy (TKE). The wavenumber spectra of both streamwise and crosswind velocity components were examined. The result provided the first quantitative estimate of the scales at which energy is injected into the turbulence by the blades and tower. An inertial subrange was observed at all heights, and it was determined that the tower redistributed TKE to a wider range of scales.ud
机译:进行了实验研究,以研究模型水平轴风力涡轮机(HAWT)在近尾流区的平均和湍流特性,转子直径D = 0.15 m。最新的粒子图像测速技术(PIV)用于测量水平面中的二维速度场,该速度场在上游0.15 D和下游0.7 D之间延伸。在三个垂直位置(z = 0.185 m,0.135 m和0.05 m)进行了测量,以考虑叶片,支撑塔架和叶片以及塔架本身引起的尾流扰动。风速的变化使叶尖速度比(λ)的范围在3.5-4.25之间,弦雷诺数在1900-2500之间。 ud根据转子的角度配置开发了相位平均算法,以计算各种相位平均流量。结果以集合平均和相位平均的形式表示。相平均速度不足的结果确定了靠近单个叶片的加速流区域以及由于流分离而导致的较低动量的局部区域。通过湍流强度的分布证实了叶片尾旋涡度强度与湍流增加之间的相关性。雷诺应力的分布图表明,紧挨叶片和塔筒下游的应力显着增强,表明湍动能(TKE)的产生增加。检查了沿气流速度和逆风速度分量的波数谱。结果为叶片和塔筒将能量注入湍流的尺度提供了第一定量估计。在所有高度都观察到一个惯性子范围,并确定该塔将TKE重新分配到更大的比例范围。

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    Tom Kevin;

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  • 年度 2010
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