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用于振动声学模拟的非均匀湍流边界层壁面压力场合成

Synthesis of wall pressure fields of non-homogeneous turbulent boundary layers for vibroacoustic simulations.

作者信息

Guillon Corentin, Redon Emmanuel, Maxit Laurent

机构信息

Univ Lyon, INSA Lyon, LVA, EA677, 25 bis av. Jean Capelle, 69621 Villeurbanne, France.

Université de Bourgogne, ESIREM, 9 Av. Alain Savary, BP 47 870, F-21078 Dijon, France.

出版信息

J Acoust Soc Am. 2022 Feb;151(2):1039. doi: 10.1121/10.0009368.

Abstract

In this paper, a numerical process is presented for predicting the response of vibrating structures excited by a non-homogeneous turbulent boundary layer. This one is based on the synthesis of different realizations of the random pressure fluctuations that can be introduced as loading of a vibroacoustic model. The vibratory response is finally deduced by averaging together the responses of the different loads. As a first approach, the pressure fluctuations of the non-homogeneous turbulent boundary layer can be generated separately for different sub-areas of the structure by using the uncorrelated wall plane waves technique and mean boundary layer parameters. An extension of this basic approach consists in taking into account the interaction between the sub-areas and a refinement of the sub-area decomposition. Wall pressure fluctuations related to a continuous evolution of the boundary layer can then be generated and introduced in the vibroacoustic model. The accuracy of the proposed approach is studied on a rectangular panel excited on one side by a growing fully turbulent boundary layer triggered at one edge of the plate. Comparisons with the spatial approach and the wavenumber approach using the sub-area decomposition technique are proposed. Interests of the proposed approach in terms of accuracy and computing times are discussed.

摘要

本文提出了一种数值方法,用于预测由非均匀湍流边界层激发的振动结构的响应。该方法基于对随机压力波动的不同实现进行合成,这些波动可作为振动声学模型的载荷引入。最终通过对不同载荷的响应进行平均来推导振动响应。作为第一步,可以使用不相关的壁面平面波技术和平均边界层参数,为结构的不同子区域分别生成非均匀湍流边界层的压力波动。这种基本方法的扩展包括考虑子区域之间的相互作用以及细化子区域分解。然后可以生成与边界层连续演化相关的壁面压力波动,并将其引入振动声学模型。在一块矩形板上进行了研究,该板的一侧由在板的一个边缘触发的不断发展的完全湍流边界层激发,以此来研究所提方法的准确性。还将所提方法与使用子区域分解技术的空间方法和波数方法进行了比较。讨论了所提方法在准确性和计算时间方面的优势。

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