首页> 外文期刊>Energies >Combining Unsteady Blade Pressure Measurements and a Free-Wake Vortex Model to Investigate the Cycle-to-Cycle Variations in Wind Turbine Aerodynamic Blade Loads in Yaw
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Combining Unsteady Blade Pressure Measurements and a Free-Wake Vortex Model to Investigate the Cycle-to-Cycle Variations in Wind Turbine Aerodynamic Blade Loads in Yaw

机译:结合非稳态叶片压力测量和自由涡旋模型来研究偏航中风力涡轮机气动叶片载荷的周期变化

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Prediction of the unsteady aerodynamic flow phenomenon on wind turbines is challenging and still subject to considerable uncertainty. Under yawed rotor conditions, the wind turbine blades are subjected to unsteady flow conditions as a result of the blade advancing and retreating effect and the development of a skewed vortical wake created downstream of the rotor plane. Blade surface pressure measurements conducted on the NREL Phase VI rotor in yawed conditions have shown that dynamic stall causes the wind turbine blades to experience significant cycle-to-cycle variations in aerodynamic loading. These effects were observed even though the rotor was subjected to a fixed speed and a uniform and steady wind flow. This phenomenon is not normally predicted by existing dynamic stall models integrated in wind turbine design codes. This paper couples blade pressure measurements from the NREL Phase VI rotor to a free-wake vortex model to derive the angle of attack time series at the different blade sections over multiple rotor rotations and three different yaw angles. Through the adopted approach it was possible to investigate how the rotor self-induced aerodynamic load fluctuations influence the unsteady variations in the blade angles of attack and induced velocities. The hysteresis loops for the normal and tangential load coefficients plotted against the angle of attack were plotted over multiple rotor revolutions. Although cycle-to-cycle variations in the angles of attack at the different blade radial locations and azimuth positions are found to be relatively small, the corresponding variations in the normal and tangential load coefficients may be significant. Following a statistical analysis, it was concluded that the load coefficients follow a normal distribution at the majority of blade azimuth angles and radial locations. The results of this study provide further insight on how existing engineering models for dynamic stall may be improved through the integration of stochastic models to be able to account for the cycle-to-cycle variability in the unsteady wind turbine blade loads under yawed conditions.
机译:风力涡轮机上不稳定的空气流动现象的预测具有挑战性,并且仍然存在相当大的不确定性。在偏航的转子条件下,由于叶片的前进和后退作用以及在转子平面下游产生的偏斜涡旋尾流的发展,风力涡轮机叶片受到不稳定的流动条件。在偏航条件下在NREL VI阶段转子上进行的叶片表面压力测量表明,动态失速会导致风力涡轮机叶片在空气动力负载方面经历明显的周期变化。即使转子受到固定速度和均匀而稳定的风流,也观察到这些效果。集成在风力发电机设计规范中的现有动态失速模型通常无法预测这种现象。本文将来自NREL VI阶段转子的叶片压力测量结果耦合到自由苏醒涡模型,以得出在多个转子旋转和三个不同偏航角下不同叶片部分的迎角时间序列。通过采用的方法,有可能研究转子自感​​应的空气动力负载波动如何影响叶片迎角和感应速度的非稳定变化。相对于迎角绘制的法向和切向负载系数的磁滞回线是在多个转子旋转上绘制的。尽管发现在不同叶片径向位置和方位角位置上攻角的逐周期变化相对较小,但法向和切向载荷系数的相应变化可能很大。经过统计分析,得出的结论是,在大多数叶片方位角和径向位置处,载荷系数遵循正态分布。这项研究的结果提供了关于如何通过整合随机模型来改善动态失速的现有工程模型的进一步见解,从而能够解决偏航条件下非定常风力涡轮机叶片负载中的逐周期变化。

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