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Modelling of jet noise: a perspective from large-eddy simulations

机译:射流噪声建模:大涡模拟的视角

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摘要

In the last decade, many research groups have reported predictions of jet noise using high-fidelity large-eddy simulations (LES) of the turbulent jet flow and these methods are beginning to be used more broadly. A brief overview of the publications since the review by Bodony & Lele (2008, AIAA J. >56, 346–380) is undertaken to assess the progress and overall contributions of LES towards a better understanding of jet noise. In particular, we stress the meshing, numerical and modelling advances which enable detailed geometric representation of nozzle shape variations intended to impact the noise radiation, and sufficiently accurate capturing of the turbulent boundary layer at the nozzle exit. Examples of how LES is currently being used to complement experiments for challenging conditions (such as highly heated pressure-mismatched jets with afterburners) and guide jet modelling efforts are highlighted. Some of the physical insights gained from these numerical studies are discussed, in particular on crackle, screech and shock-associated noise, impingement tones, acoustic analogy models, wavepackets dynamics and resonant acoustic waves within the jet core. We close with some perspectives on the remaining challenges and upcoming opportunities for future applications.This article is part of the theme issue ‘Frontiers of aeroacoustics research: theory, computation and experiment’.
机译:在过去的十年中,许多研究小组已经报告了使用湍流射流的高保真大涡模拟(LES)对射流噪声的预测,并且这些方法开始被更广泛地使用。自Bodony&Lele(2008,AIAA J. > 56 ,346–380)进行审查以来,对出版物进行了简要概述,以评估LES对更好理解喷气噪声的进展和总体贡献。 。特别是,我们强调网格划分,数值和建模方面的进步,这些进展使得能够对旨在影响噪声辐射的喷嘴形状变化进行详细的几何表示,并在喷嘴出口处充分准确地捕获了湍流边界层。当前着重介绍了如何使用LES来补充具有挑战性的条件(例如,带有加力口的高温加热压力不匹配喷嘴)和引导喷嘴建模工作的示例。讨论了从这些数值研究中获得的一些物理见解,尤其是在裂纹,刺耳声和与冲击相关的噪声,撞击音,声学类比模型,波包动力学和射流核心内的共振声波方面。本文以“航空声学研究的前沿:理论,计算和实验”为主题,其中部分内容涉及“剩余的挑战和未来的应用前景”。

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