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首页> 外文期刊>Noise & vibration bulletin >AERODYNAMIC NOISE CHARACTERIZATION OF A FULL-SCALE WIND TURBINE THROUGH HIGH-FREQUENCY SURFACE PRESSURE MEASUREMENTS
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AERODYNAMIC NOISE CHARACTERIZATION OF A FULL-SCALE WIND TURBINE THROUGH HIGH-FREQUENCY SURFACE PRESSURE MEASUREMENTS

机译:高频表面压力测量的大型风轮机气动噪声特性

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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 noise, 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 an 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 28 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流入噪声和尾随噪声的来源高度相关,因此这项工作有助于更深入地了解风力涡轮机的噪声。这项研究包括对在实验活动期间获得的测量数据进行分析和解释,该实验涉及2 MW直径为80 m转子的风力涡轮机,以及在风洞中测试的机翼截面的测量。涡轮机配备了广泛的设备,以监控流入旋转叶片的局部流量。另外,在28 m长的刀片的一部分上安装了50个相对于刀片表面齐平安装的麦克风。将表面压力频谱的测量结果与两个工程模型的结果进行比较,以得出后缘噪声和湍流流入噪声。测得的压力波动与局部流入角有关,并且还与风管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。测量数据和模型结果之间的比较显示了大气湍流的影响。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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