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Lift Limit of Horizontal Axis Wind Turbine

机译:水平轴风力涡轮机的提升极限

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摘要

The lift coefficient of any wind turbine must have highest limit. In this paper, an analytical expression of lift coefficient associated with tip-speed ratio and lift-drag ratio of airfoil of wind turbine with ideal chord has been deduced by integrating along the blade wingspan using the blade element - momentum theory, which can be used for pre-estimating lift coefficient of actual wind turbine in design. Further, considering ideal fluid environment (the drag coefficient is close to 0 ), an expression of the highest performance of lift only associated with tip-speed ratio has been deduced too, which is the highest boundary of lift coefficient of any actual wind turbine with same tip-speed ratio. The results show that for the wind turbine in steady state, there is a theoretical limit of the lift coefficient, 0.57795, which is the highest boundary that any actual wind turbine can not be crossed; if the tip-speed ratio is greater than 6 and lift-drag ratio less than 200, the lift coefficient is unlikely to exceed 0.2.
机译:任何风力涡轮机的升力系数必须具有最高限制。在本文中,通过沿着叶片元件沿着刀片元件 - 动量理论集成了与理想和平弦的翼速比与翼型的尖端速度比和升降比的分析表达,其中可以使用叶片翅膀 - 动量理论用于设计实际风力涡轮机的预估算系数。此外,考虑到理想的流体环境(拖动系数接近0),也已经推导出仅与尖端速比相关的升力性能的最高性能的表达,这是任何实际风力涡轮机的提升系数的最高边界相同的尖端速度比。结果表明,对于风力涡轮机处于稳态,有升力系数的理论极限,0.57795,这是任何实际风力涡轮机无法交叉的最高边界;如果尖端速度比大于6并且升力比小于200,则升力系数不太可能超过0.2。

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