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The effect of rotation on the boundary layer of a wind turbine blade

机译:旋转对风力涡轮机叶片边界层的影响

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摘要

Design and analysis methods for wind turbines are presently based on relatively simple models of rotor blade aerodynamics, such as 2-D blade element/momentum theory (BEMT). Field investigations over the past few years have shown discrepancies between predicted and measured performance, owing to the effect of rotation on the wind turbine blade boundary layer disribution. The present papaer is aimed at describing a fundamental phenomenon: the effect of rotation. The present paper is aimed at describing a fundamental phenomenon: the effect of totation on the blade boundary layer of a wind turbine. In this paper, 3-D incompressible steady momentum integral boundary layer equations are employed to study this complex problem. By solving the 3-D integral boundary layer equations with the assumed velocity profies and a closure model (including both laminar and turbulent boundary layer models), theeffects of rotation on blade boundary layers are investigated. Several key parameters, such as separation position and momentum thickness, are calculated and compared due to totation and the separation point is delayed as a result of increasing rotation speed or decreasing blade spanwise position. Possible modifications that should be considered to the existing 2-D BEMT method are suggested.
机译:当前,用于风力涡轮机的设计和分析方法基于转子叶片空气动力学的相对简单的模型,例如二维叶片元件/动量理论(BEMT)。过去几年的实地调查表明,由于旋转对风力涡轮机叶片边界层分布的影响,预测性能和实测性能之间存在差异。本论文旨在描述一个基本现象:旋转的影响。本文旨在描述一种基本现象:扭转对风力涡轮机叶片边界层的影响。本文采用3-D不可压缩稳态动量积分边界层方程来研究这一复杂问题。通过用假定的速度特性和闭合模型(包括层流和湍流边界层模型)求解3-D积分边界层方程,研究了旋转对叶片边界层的影响。几个关键参数,例如分离位置和动量厚度,会由于扭转而被计算和比较,而分离点由于转速增加或叶片翼展方向位置减小而被延迟。建议对现有的二维BEMT方法应考虑的可能修改。

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