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Estimating the angle of attack from blade pressure measurements on the National Renewable Energy Laboratory phase VI rotor using a free wake vortex model : yawed conditions

机译:使用自由尾流涡流模型估算国家可再生能源实验室VI期转子上的叶片压力测量值的迎角:偏航条件

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摘要

Wind turbine design codes for calculating blade loads are usually based on a blade element momentum (BEM) approach. Since wind turbine rotors often operate in off-design conditions, such as yawed flow, several engineering methods have been developed to take into account such conditions. An essential feature of a BEM code is the coupling of local blade element loads with an external (induced) velocity field determined with momentum theory through the angle of attack. Local blade loads follow directly from blade pressure measurements as performed in the National Renewable Energy Laboratory (NREL) phase IV campaign, but corresponding angles of attack cannot (on principle) be measured. By developing a free wake vortex method using measured local blade loads, time-dependent angle of attack and induced velocity distributions are reconstructed. In a previous paper, a method was described for deriving such distributions in conjunction with blade pressure measurements for the NREL phase VI wind turbine in axial (non-yawed) conditions. In this paper, the same method is applied to investigate yawed conditions on the same turbine. The study considered different operating conditions in yaw in both attached and separated flows over the blades. The derived free wake geometry solutions are used to determine induced velocity distributions at the rotor blade. These are then used to determine the local (azimuth time dependent) angle of attack, as well as the corresponding lift and drag for each blade section. The derived results are helpful to develop better engineering models for wind turbine design codes.
机译:用于计算叶片载荷的风力涡轮机设计规范通常基于叶片元素动量(BEM)方法。由于风力涡轮机转子通常在偏离设计的条件下运行,例如偏航,因此已经开发出多种工程方法来考虑这种条件。 BEM代码的基本特征是将局部叶片单元载荷与通过迎角通过动量理论确定的外部(感应)速度场耦合。叶片的局部载荷直接来自于国家可再生能源实验室(NREL)第四阶段战役中进行的叶片压力测量,但是(原则上)无法测量相应的迎角。通过开发使用测量的局部叶片载荷的自由尾流涡旋方法,可以重构随时间变化的迎角和感应速度分布。在先前的论文中,描述了一种用于在轴向(非偏航)条件下结合NREL VI阶段风力涡轮机叶片压力测量来推导此类分布的方法。在本文中,将相同的方法应用于研究同一涡轮机的偏航条件。该研究考虑了叶片上附着的和分离的流动中偏航的不同操作条件。导出的自由尾流几何解用于确定转子叶片处的感应速度分布。然后将这些值用于确定局部(与方位角时间有关)的迎角,以及每个叶片部分的相应升力和阻力。得出的结果有助于为风机设计规范开发更好的工程模型。

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