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Effect of Turbulence Loading on a 2-D Aerofoil

机译:湍流载荷对二维翼型的影响

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In the present 2-D study, experimental and numerical simulation approaches have been carried out to investigate the significance of turbulence (turbulence intensity and length scale) on a wind turbine blade performance. The aim was to provide an adequate insight into the turbulent flow and its effect on the wind turbine blade. An experimental investigation was performed in a tunnel in the University of Manchester with a 1 m~2 cross section and length of 6m. The flow turbulent characteristics have been established and maintained along the tunnel using three conventional obstacles (grid, elliptic vortex generator and a number of wooden cubes) and combination of the above. The flow features have been measured using cross hot wire anemometry. The effect of different flow patterns has been quantified on an NACA4705 aerofoil using force balance technique for a range of low Reynolds numbers (4×10~4-7×10~4). In parallel to the experimental effort, a simulation approach has been conducted by means of two commercial packages, Fluent and Star-CD. The results confirmed the significant effect of turbulent intensity on aerofoil performance.
机译:在当前的二维研究中,已经进行了实验和数值模拟方法以研究湍流(湍流强度和长度尺度)对风力涡轮机叶片性能的重要性。目的是充分了解湍流及其对风力涡轮机叶片的影响。在曼彻斯特大学的一个隧道中进行了实验研究,该隧道的横截面为1 m〜2,长度为6m。使用三个常规障碍物(格栅,椭圆形涡流发生器和许多木立方体)以及以上各项的组合,已经建立并维持了沿隧道的流动湍流特性。流动特征已使用交叉热线风速仪进行了测量。使用力平衡技术,在一定范围的低雷诺数(4×10〜4-7×10〜4)下,已对NACA4705机翼上不同流动模式的影响进行了量化。与实验工作并行的是,已经通过两个商业软件包Fluent和Star-CD进行了模拟方法。结果证实了湍流强度对机翼性能的显着影响。

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