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Aeroacoustics of Darrieus wind turbine

机译:Darrieus风力发电机的航空声学

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The objective of this paper is to validate two different numerical methods for noise prediction of the H-Darrieus wind turbine using a complementary approach consisting of experimental measurements and numerical simulations. The acoustic measurements of a model scale rotor were performed in an anechoic wind tunnel. This data is the basis for the validation of the computational aeroacoustic simulations. Thereby, we have applied two different numerical schemes for noise prediction using hybrid methods. As usual in hybrid aeroacoustic approaches, flow field and acoustic calculations are carried out in separate software packages. For both schemes the time-dependent turbulent flow field is solved with Scale-Adaptive Simulation. The two schemes then differ in how the location of the acoustic sources and their propagation is calculated. In the first scheme the acoustic source terms are computed according to Lighthill's acoustic analogy which gives source terms located on the original CFD grid. These source terms are projected onto a coarser acoustic grid on which Lighthill's inhomogenous wave equation is solved by the Finite Element (FE) method. The second scheme uses the Ffowcs Williams-Hawkines (FW-H) method which is based on a free field Green's function. The scheme uses a porous integration surface and implements an advanced time formulation. Both methodologies are compared with experimental data.
机译:本文的目的是使用由实验测量和数值模拟组成的补充方法,验证两种不同的数值方法来预测H-Darrieus风力发电机的噪声。模型模型转子的声学测量是在无声风洞中进行的。该数据是验证航空声学模拟的基础。因此,我们使用混合方法将两种不同的数值方案应用于噪声预测。与混合航空声学方法一样,流场和声学计算在单独的软件包中进行。对于这两种方案,都通过比例自适应仿真解决了与时间有关的湍流场。然后,这两种方案在如何计算声源的位置及其传播方面有所不同。在第一种方案中,声源项是根据Lighthill的声学类比法计算的,该模拟给出了位于原始CFD网格上的源项。这些源项被投影到一个较粗糙的声学网格上,在该网格上,Lighthill的不均匀波动方程通过有限元(FE)方法求解。第二种方案使用基于自由场格林函数的Ffowcs Williams-Hawkines(FW-H)方法。该方案使用多孔集成表面并执行高级时间公式。两种方法都与实验数据进行了比较。

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