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Aerodynamic noise characterization of a full-scale wind turbine through high-frequency surface pressure measurements

机译:通过高频表面压力测量来表征全尺寸风力涡轮机的空气动力学噪声

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The aim of this work is to investigate and characterize the high-frequency surface pressure fluctuations on a full-scale wind turbine blade and in particular the influence of the atmospheric turbulence. As these fluctuations are highly correlated to the sources of both turbulent inflow noise and trailing edge noise, recognized to be the two main sources of noise from wind turbines, this work contributes to a more detailed insight into noise from wind turbines. The study comprises analysis and interpretation of measurement data that were acquired during an experimental campaign involving a 2 MW wind turbine with a 80 m diameter rotor as well as measurements of an airfoil section tested in a wind tunnel, The turbine was extensively equipped in order to monitor the local inflow onto the rotating blades. Further a section of the 38 m long blade was instrumented with 50 microphones flush-mounted relative to the blade surface, The measurements of surface pressure spectra are compared with the results of two engineering models for trailing edge noise and for turbulent inflow noise. The measured pressure fluctuations are related to the local inflow angle and are also compared to measurements in a wind tunnel on a copy of the blade section of the full scale blade. Computational Fluid Dynamics calculations were conducted to investigate the influence of the inflow conditions on the airfoil and blade sections aerodynamics and aeroacoustics, Comparisons between measurement data and model results show the influence of atmospheric turbulence. The different noise generation mechanisms can be identified and the influence of various parameters can be consistently reproduced by the models.
机译:这项工作的目的是研究和表征全尺寸风力涡轮机叶片上的高频表面压力波动,尤其是大气湍流的影响。由于这些波动与湍流的流入噪声和后缘噪声(都被认为是风力涡轮机的两个主要噪声源)高度相关,因此这项工作有助于更深入地了解风力涡轮机的噪声。该研究包括对实验数据的分析和解释,该实验数据涉及2 MW直径为80 m转子的风力涡轮机,以及在风洞中测试的翼型截面的测量。监控流入旋转叶片的局部流量。此外,在38 m长的叶片的一部分上安装了50个相对于叶片表面齐平安装的麦克风。将表面压力谱的测量结果与两个工程模型的后缘噪声和湍流流入噪声的结果进行了比较。测得的压力波动与局部入流角有关,并且还与风洞中满刻度叶片的叶片部分副本上的测量值进行比较。进行了计算流体动力学计算,以研究流入条件对翼型和叶片截面的空气动力学和空气声学的影响,测量数据与模型结果的比较表明了大气湍流的影响。可以识别不同的噪声生成机制,并且可以通过模型一致地再现各种参数的影响。

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