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Validation of the numerical simulations of flow around a scaled-down turbine using experimental data from wind tunnel

机译:使用风洞的实验数据验证缩小涡轮机周围流动的数值模拟

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Aerodynamic characteristic of a small scale wind turbine under the influence of an incoming uniform wind field is studied using k-omega Shear Stress Transport turbulence model. Firstly, the lift and drag characteristics of the blade section consisting of S826 airfoil is studied using 2D simulations at a Reynolds number of 1x10(5). After that, the full turbine including the rotational effects of the blade is simulated using Multiple Reference Frames (MRF) and Sliding Mesh Interface (SMI) numerical techniques. The differences between the two techniques are quantified. It is then followed by a detailed comparison of the turbine's power/thrust output and the associated wake development at three tip speeds ratios (lambda = 3, 6, 10). The phenomenon of blockage effect and spatial features of the flow are explained and linked to the turbines power output Validation of wake profiles patterns at multiple locations downstream is also performed at each lambda. The present work aims to evaluate the potential of the numerical methods in reproducing wind tunnel experimental results such that the method can be applied to full-scale turbines operating under realistic conditions in which observation data is scarce or lacking.
机译:采用K-Omega剪切应力输送湍流模型研究了进入均匀风电场影响下的小型风力涡轮机的空气动力学特性。首先,在雷诺数为1×10(5)的雷诺数,研究由S826翼型组成的叶片部分的提升和拖曳特性。之后,使用多个参考帧(MRF)和滑动网格接口(SMI)数值技术来模拟包括刀片的旋转效果的全涡轮机。量化了两种技术之间的差异。然后,在三个尖端速度比(Lambda = 3,6,10)上详细比较涡轮机的电源/推力输出和相关的唤醒开发。对流动的堵塞效果和空间特征的现象被解释和链接到涡轮机电力输出验证在每个λ下游的多个位置处的多个位置的模式。本作者旨在评估在再现风洞实验结果中的数值方法的潜力,使得该方法可以应用于在实际条件下运行的全尺寸涡轮机,其中观察数据稀缺或缺乏。

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