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Numerical Simulation of Influence with Surface contamination on Aerodynamic Performance of Dedicated Wind Turbine Airfoil

机译:用表面污染对专用风力涡轮机翼型空气动力学性能影响的数值模拟

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A Numerical simulation on the influence of airfoil surface contamination on the aerodynamic performance of wind turbines was performed. It chose the dedicated wind turbine airfoil as the research object. The k-ω Shear Stress Transmission (SST) turbulence model was selected for CFD calculation. The roughness height which arranged evenly on the airfoil was changed from 0.03mm to 2.0mm to obtain the sensitive roughness. The airfoil was divided into 18 sections for analyzing the effect on the lift & the drag coefficient, due to various locations of sensitive roughness. By comparing the result computed by XFOIL and CFD calculation, it can be known this airfoil's sensitive locations in suction surface and pressure surface. The sensitive locations in suction surface were 53% and 92% from the chord line towards the leading edge, while 44% and 88% in pressure surface. The sensitive roughness in sensitive locations delayed the location of the transition point.
机译:进行了对翼型表面污染对风力涡轮机空气动力学性能的数值模拟。它选择了专门的风力涡轮机翼型作为研究对象。选择了K-ω剪切应力传输(SST)湍流模型用于CFD计算。均匀地布置在翼型上的粗糙度高度从0.03mm变为2.0mm以获得敏感的粗糙度。由于各种敏感粗糙度的位置,将翼型分成18个部分,用于分析升力和拖曳系数的效果。通过比较XFoil和CFD计算计算的结果,可以知道该翼型在吸入表面和压力表面中的敏感位置。吸入表面的敏感位置是从弦线朝向前缘的53%和92%,而压力表面的44%和88%。敏感位置的敏感粗糙度延迟了过渡点的位置。

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