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Experimental study of the wake characteristics of an axial flow hydrokinetic turbine at different tip speed ratios

机译:不同尖端速度比下轴流水动力学涡轮机的试验研究

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The wake characteristics of an axial flow hydrokinetic turbine were investigated for various tip speed ratios using velocity measurements and a flow visualization technique. The experimental results showed that the structures of the wake within six rotor diameters downstream of the turbine are significantly affected by a change in the tip speed ratio. As a tip speed ratio decreases, the core region of the wake that is featured by low axial velocity near the turbine rotor hub became more unstable, producing higher turbulence levels in the radial and azimuthal directions. It resulted in different growth rates of the shear layer that expands from the core region toward the outer part of the wake and that interacts with the tip vortices to trigger wake meandering. It turns out that the swirl number of the wake is a key factor that determines the stability of the core region in the near wake region. At locations more than six rotor diameters away from the turbines, the mean and turbulence characteristics became nearly independent of the change in the tip speed ratio. This was due to large-scale turbulent mixing whose size was in the order of the rotor diameter.
机译:使用速度测量和流动可视化技术研究了各种尖端速度比的轴流式流动涡轮机的唤醒特性。实验结果表明,在涡轮机下游的六个转子直径内的唤醒结构受到尖端速比的变化的显着影响。作为尖端速度比降低,涡轮机转子毂附近的低轴向速度特征的尾部的芯区域变得更加不稳定,在径向和方位角方向上产生更高的湍流水平。它导致剪切层的不同生长速率,其从芯区域扩展到唤醒的外部并且与尖端涡旋相互作用以触发曲目曲折。事实证明,唤醒的旋流数是确定靠近唤醒区域中核心区域的稳定性的关键因素。在远离涡轮机的多于六个转子直径的位置,平均和湍流特性几乎与尖端速度比的变化几乎无关。这是由于大规模湍流混合,其尺寸为转子直径的顺序。

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