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EXPERIMENTAL NUMERICAL INVESTIGATION OF INFLOW TURBULENCE ON THE PERFORMANCE OF WIND TURBINE AIRFOILS

机译:进风湍流对风轮机翼型性能的实验与数值研究

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Wind turbine blade design is currently based on the combination of a plurality of airfoil sections along the rotorblade span. The two-dimensional airfoil characteristics are usually measured with wind tunnel experiments or computed by means of numerical simulation codes. The general airfoil input for the calculation of the rotorblade power characteristics as well as the subsequent aerodynamic and aeroelastic loads are based on these two-dimensional airfoil characteristics. In this paper, the effects of inflow turbulence and wind tunnel test measurement deviations are investigated and discussed, to allow considerations of such effects in the rotorblade design process. The results of CFD simulations with various turbulence models are utilized in combination with wind tunnel measurements in order to assess the impact of such discrepancies. It seems that turbulence, airfoil surface roughness and early transition effects are able to contribute significantly to the uncertainty and scattering of measurements. Various wind tunnel facilities generate different performance characteristic curves, while grid-generated turbulence is generally not included in the wind tunnel measurements during airfoil characterization. Furthermore the correlation of grid-generated wind tunnel turbulence with the atmospheric turbulence time and length scales is not easily achieved. All the aforementioned uncertainties can increase the performance scattering of current wind turbine blade designs as well as the generated aeroelastic loads. A brief assessment of the effect of such uncertainties on wind turbine performance is given at the last part of this work by means of BEM simulations on a wind turbine blade.
机译:当前,风力涡轮机叶片设计基于沿着转子叶片跨度的多个翼型部分的组合。二维翼型特性通常通过风洞实验测量或通过数值模拟代码进行计算。用于计算转子叶片功率特性以及随后的气动和气动弹性载荷的通用翼型输入均基于这些二维翼型特性。在本文中,对流入湍流和风洞测试测量偏差的影响进行了研究和讨论,以便在旋翼桨叶设计过程中考虑这种影响。将具有各种湍流模型的CFD模拟结果与风洞测量结合使用,以评估此类差异的影响。湍流,机翼表面粗糙度和早期过渡效应似乎可以显着地影响测量的不确定性和分散性。各种风洞设施会生成不同的性能特征曲线,而在机翼表征期间,风洞测量中通常不包括网格生成的湍流。此外,不容易实现电网产生的风洞湍流与大气湍流时间和长度尺度的相关性。所有上述不确定性都会增加当前风力涡轮机叶片设计的性能分散性以及所产生的气动弹性载荷。在这项工作的最后部分,通过对风力涡轮机叶片的BEM仿真,对此类不确定性对风力涡轮机性能的影响进行了简要评估。

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