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The influence of blade curvature and helical blade twist on the performance of a vertical-axis wind turbine

机译:叶片曲率和螺旋叶片扭曲对垂直轴风力发电机性能的影响

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摘要

Accurate aerodynamic modeling of vertical-axis wind turbines poses a significant challenge, but is essential if the performance of such turbines is to be predicted reliably. The rotation of the turbine induces large variations in the angle of attack of its blades that canmanifest as dynamic stall. In addition, interactions between the blades of the turbine and the wake that they produce can exacerbate dynamic stall and result in impulsive changes to the aerodynamic loading on the blades. The Vorticity Transport Model has been used to simulate the aerodynamic performance and wake dynamics of vertical-axis wind turbines with straight-bladed, curved-bladed and helically twisted configuration. It is known that vertical-axis wind turbines with either straight or curved blades deliver torque to their shaft that fluctuates at the blade passage frequency of the rotor. In contrast, a rotor with helically twisted blades delivers a relatively steady torque to the shaft. In the present paper, the interactions between helically twisted blades and the vortices within their wake are shown to result in localized perturbations to the aerodynamic loading on the rotor that can disrupt the otherwise relatively smooth power output that is predicted by simplistic aerodynamic tools that do not model the wake to sufficient fidelity. Furthermore, vertical-axis wind turbines with curved blades are shown to be somewhat more susceptible to local dynamic stall than turbines with straight blades.
机译:垂直轴风力涡轮机的精确空气动力学建模提出了重大挑战,但对于要可靠地预测此类涡轮机的性能而言,必不可少。涡轮机的旋转会引起其叶片攻角的较大变化,这可以表现为动态失速。另外,涡轮机叶片与叶片产生的尾流之间的相互作用会加剧动态失速,并导致叶片上的空气动力学负载发生脉冲式变化。涡度传输模型已用于模拟具有直叶,弯叶和螺旋扭曲配置的垂直轴风力涡轮机的空气动力学性能和尾流动力学。已知具有直叶片或弯曲叶片的垂直轴风力涡轮机将转矩传递到其轴,该转矩以转子的叶片通过频率波动。相反,具有螺旋形扭曲叶片的转子向轴传递相对稳定的扭矩。在本文中,螺旋形螺旋叶片和涡流之间的涡流之间的相互作用被显示为导致对转子上空气动力负载的局部扰动,这会破坏原本相对平稳的动力输出,而这种动力输出是由简单的空气动力工具预测的,而不是对唤醒建模,使其具有足够的保真度。此外,具有弯曲叶片的垂直轴风力涡轮机显示出比具有直线叶片的涡轮机更容易受到局部动态失速的影响。

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