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Turbulent Flow Inside and Above a Wind Farm: A Wind-Tunnel Study

机译:风电场内部和上方的湍流:风洞研究

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摘要

Wind-tunnel experiments were carried out to better understand boundary layer effects on the flow pattern inside and above a model wind farm under thermally neutral conditions. Cross-wire anemometry was used to characterize the turbulent flow structure at different locations around a 10 by 3 array of model wind turbines aligned with the mean flow and arranged in two different layouts (inter-turbine separation of 5 and 7 rotor diameters in the direction of the mean flow by 4 rotor diameters in its span). Results suggest that the turbulent flow can be characterized in two broad regions. The first, located below the turbine top tip height, has a direct effect on the performance of the turbines. In that region, the turbulent flow statistics appear to reach equilibrium as close as the third to fourth row of wind turbines for both layouts. In the second region, located right above the first one, the flow adjusts slowly. There, two layers can be identified: an internal boundary layer where the flow is affected by both the incoming wind and the wind turbines, and an equilibrium layer, where the flow is fully adjusted to the wind farm. An adjusted logarithmic velocity distribution is observed in the equilibrium layer starting from the sixth row of wind turbines. The effective surface roughness length induced by the wind farm is found to be higher than that predicted by some existing models. Momentum recovery and turbulence intensity are shown to be affected by the wind farm layout. Power spectra show that the signature of the tip vortices, in both streamwise and vertical velocity components, is highly affected by both the relative location in the wind farm and the wind farm layout.
机译:进行风洞实验是为了更好地了解边界层对热中性条件下模型风场内部和上方的流型的影响。交叉线风速仪用于表征围绕10 x 3阵列风轮机的不同位置处的湍流结构,该风轮机与平均风量对齐并布置在两种不同的布局中(沿方向将涡轮直径分开5和7)平均流量乘以其跨度中的4个转子直径)。结果表明,湍流可以在两个广泛的区域进行表征。第一个位于涡轮机顶部尖端高度以下,直接影响涡轮机的性能。在该区域中,两种布局的湍流统计量似乎都达到了与第三至第四排风力涡轮机接近的平衡。在位于第一个区域正上方的第二个区域中,流量调整缓慢。在那里,可以识别出两层:内部边界层,其中流量受到传入的风力和风力涡轮机的影响;以及平衡层,其中流量完全适应风电场。从第六排风力涡轮机开始,在平衡层中观察到调整后的对数速度分布。发现由风电场引起的有效表面粗糙度长度要比某些现有模型预测的长度高。动量恢复和湍流强度显示受风电场布局的影响。功率谱表明,在气流速度和垂直速度分量上,尖端涡旋的特征都受到风电场中相对位置和风电场布局的极大影响。

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