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A model to include turbulence-turbulence interaction in the prediction of trailing edge far field noise for high angles of attack or slightly separated flow

机译:在高攻角或略微​​分离流动的后缘远场噪声预测中包括湍流-湍流相互作用的模型

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摘要

The most dominant noise source of modern wind turbines is considered to be trailing edge (TE) noise. TE noise increases with increasing angle of attack of the flow. For wind turbine development it is hence crucial to predict TE noise for high angles of attack up to slightly separated flow. It results from wall pressure fluctuations induced by turbulent vortices in the boundary layer. The source term for the pressure fluctuations consists of two terms, the interaction of the mean shear with the turbulence and the turbulence-turbulence interaction (TTI). TTI is neglected in the commonly used TE noise prediction model by Blake, resulting in a strong dependency of the model on the wall normal mean velocity gradient. With increasing angle of attack this wall normal gradient of the boundary layer diminishes. Hence the TTI of the source equation has to be taken into account in order to achieve reliable predictions towards higher angles of attack. Here a new simplified-analytical model including the TTI, based on the model deduction by Blake, is presented and compared to experimental data. It is found that the prediction quality for high angles of attack and slight TE separation can be improved with the new model. (C) 2019 Elsevier Ltd. All rights reserved.
机译:现代风力涡轮机最主要的噪声源被认为是后缘(TE)噪声。 TE噪声随着流动迎角的增加而增加。因此,对于风力涡轮机的开发,预测TE噪声对于大迎角直至略微分离的气流至关重要。它是由边界层中湍流涡流引起的壁面压力波动引起的。压力波动的源项包括两个项,即平均剪切力与湍流的相互作用以及湍流-湍流相互作用(TTI)。布雷克(Blake)在常用的TE噪声预测模型中忽略了TTI,导致该模型强烈依赖于墙体法向平均速度梯度。随着迎角的增加,边界层的该壁的法向梯度减小。因此,必须考虑源方程的TTI,以便对更高的迎角实现可靠的预测。在此,基于布雷克的模型推导,提出了一个新的简化分析模型,其中包括TTI,并将其与实验数据进行了比较。发现使用新模型可以提高大迎角和轻微TE分离的预测质量。 (C)2019 Elsevier Ltd.保留所有权利。

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