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Actuator disc modelling based on aerodynamic data extraction from direct rotor modelling of the NREL Phase Ⅵ turbine

机译:基于NRELⅥ相涡轮直接转子建模中基于空气动力学数据提取的执行器盘建模

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Traditional blade element momentum (BEM) methods based on two-dimensional data are unable to accurately predict blade forces and thus are unreliable when used in actuator discs to predict wind turbine wake profiles. This can be circumvented by extracting relevant force and velocity data from direct modelling simulations or experiments, which are almost certainly used in the design process of a wind turbine. Methods developed by Bak et al. in 1999 to extract cross-sectional aerodynamic data from wind turbines included one based on an inverse BEM method, and an actuator disc-based method, which used the exact pressure drop for each specific wind speed to create a model of pressure drop against local velocities. The present work will thus investigate the accuracy of actuator disc models based on direct rotor modelling data, by creating actuator discs through extraction of the induction factors using the methods described earlier, for the NREL Phase Ⅵ rotor.
机译:基于二维数据的传统叶片动量(BEM)方法无法准确预测叶片力,因此在致动器盘中用于预测风力涡轮机尾流轮廓时不可靠。可以通过从直接建模仿真或实验中提取相关的力和速度数据来避免这种情况,这些数据几乎可以肯定地用于风力涡轮机的设计过程中。由Bak等人开发的方法。在1999年从风力涡轮机中提取横截面空气动力学数据,包括基于逆BEM方法的数据和基于致动器圆盘的方法,该方法使用每个特定风速的精确压降来创建针对局部速度的压降模型。因此,本工作将通过使用前面所述的方法对NRELⅥ相转子通过提取感应系数来创建执行器盘,从而基于直接转子建模数据研究执行器盘模型的准确性。

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