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Piv Experimental and Numerical Study of a 2-D Airfoil for Wind Turbines

机译:风力涡轮机2-D翼型的PIV实验性和数值研究

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The 2-D airfoil of the wind turbine (NREL S809) was experimentally and numerically studied. The experiment focused on the PIV measurement of the 2-D airfoil flow field with different angles of attack under various Reynolds numbers. A lot of important and useful information was obtained. Furthermore, the experimental result was compared with CFD simulation in order to study the flow field in more detail, especially the useful graphs of the velocity vector, the data of the lift and drag, the distribution of the vortex, and separation of surface boundary layer under the different angles of attack and with different Reynolds numbers were compared and analyzed. Relatively good agreement between the experimental and numerical result was achieved.
机译:实验和数值研究了风力涡轮机(NRES S809)的2-D翼型。实验专注于2-D翼型流场的PIV测量,在各种雷诺数下具有不同的攻击角度。获得了很多重要和有用的信息。此外,将实验结果与CFD模拟进行比较,以便更详细地研究流场,尤其是速度向量的有用曲线,提升和拖动的数据,涡旋的分布以及表面边界层的分离。在不同的攻击角度下,比较和分析不同的雷诺数。实现了实验和数值结果之间的相对良好的一致性。

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