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Study on Aerodynamic Characteristics of Darrieus Vertical Axis Wind Turbines with Different Airfoil Maximum Thicknesses Through Computational Fluid Dynamics

机译:通过计算流体力学研究不同翼型最大厚度的达里厄斯垂直轴风力发电机的气动特性

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The aerodynamic characteristics of Darrieus vertical axis wind turbines (VAWTs) are affected by several geometrical parameters.Airfoil shape is one of the important factors which have not been received enough attention in the past, compared toother parameters such as solidity, number of blades, chord length, rotor diameter, pitch angle and aspect ratio. In this paper,four airfoils with varying maximum thickness (12%, 15%, 18% and 21%) are investigated by calculating the aerodynamiccharacteristics of Darrieus VAWTs using computational fluid dynamics technology. The power and torque characteristics,as well as their flow field characteristics, are analyzed. The results indicate that the power coefficient follows a trend ofCP_(_NACA 0018) > CP_(_NACA 0015) > CP_(_NACA 0021) > CP_(_NACA 0012) below an optimum TSR, while it increases with the decrease inairfoil maximum thickness beyond the optimum TSR. The optimum TSR and operational zone also increase with the decreasein airfoil maximum thickness. An optimized airfoil thickness is determined to be between 15 and 18% for a relatively highpower coefficient and appropriate optimum TSR, as well as a wider operational zone and a high efficiency band. Moreover,the airfoil maximum thickness influences the strength and region of the vorticity, as well as the interactions between bladesand shed vortex, being the main reason for the observed differences in instantaneous torque coefficient. The vorticity ofNACA 0015 model is weaker and smaller than that of NACA 0021 model when TSR is 2.0.
机译:Darrieus垂直轴风力涡轮机(VAWT)的空气动力学特性受几个几何参数的影响。与其他参数如坚固性,叶片数,弦长相比,机翼形状是过去尚未引起足够重视的重要因素之一。长度,转子直径,螺距角和长宽比。本文利用计算流体动力学技术计算了Darrieus VAWT的空气动力学特性,研究了四种具有最大厚度变化的翼型(分别为12%,15%,18%和21%)。分析了功率和转矩特性及其流场特性。结果表明,功率系数在最佳TSR以下遵循CP _(_ NACA 0018)> CP _(_ NACA 0015)> CP _(_ NACA 0021)> CP _(_ NACA 0012)的趋势,而随着翼型最大厚度的减小而超过最优值时,功率系数增加。 TSR。最佳TSR和操作区也随着翼型最大厚度的减小而增加。对于相对较高的功率系数和适当的最佳TSR,以及较宽的工作区域和高效率范围,确定的最佳翼型厚度在15%至18%之间。而且,翼型的最大厚度影响涡度的强度和区域,以及叶片与脱落涡之间的相互作用,这是观察到的瞬时转矩系数差异的主要原因。当TSR为2.0时,NACA 0015模型的涡度比NACA 0021模型的涡度弱且小。

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