二维剪切层中旋涡声的流体动力源

IF 1.2 4区 工程技术 Q3 ACOUSTICS
Yongle Du, Hangwen Yu, Yanchen Liu, Dangguo Yang
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引用次数: 0

摘要

开发先进的降噪设备需要深入了解两个基本问题:什么是真正的噪声源以及声辐射是如何产生的。精确分离流体动力学和声学波动有助于揭示答案,但在可压缩流的近场源区,对其可行性还没有达成共识。本研究提出了一种研究二维人工激发亚音速混合层中旋涡声产生动力学的方法。应用抛物化稳定方程(PSE)求解流体动力学波动,并用涡声理论预测声压。数值模拟表明,PSE解合理准确地捕捉了涡流配对,并将声学模式阻尼到可忽略的水平,并且涡流声理论恢复了声压。两种解决方案与直接模拟的良好一致性表明,实现了流体动力源的物理合理分离,可用于进一步研究涡流动力学和噪声源机制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Hydrodynamic sources of the vortex sound in a two-dimensional shear layer
Development of advanced noise reduction devices requires an in-depth understanding of two fundamental questions: what are the true noise sources and how are the acoustic radiations generated. An accurate separation of the hydrodynamic and acoustic fluctuations helps to reveal the answers, but no consensus exists on its feasibility in the near-field source region of compressible flows. This study proposes a methodology to examine the dynamics of vortex sound generation in a two-dimensional artificially excited subsonic mixing layer. The parabolized stability equation (PSE) is applied to resolve the hydrodynamic fluctuations and the vortex sound theory is used to predict the acoustic pressures. Numerical simulations show that the PSE solutions capture the vortex pairing reasonably accurately and damp the acoustic modes to a negligible level, and that the vortex sound theory recovers the acoustic pressures. Good agreement of both solutions with the direct simulations indicates that a physically reasonable separation of hydrodynamic sources is achieved and can be used to further examine the vortex dynamics and noise source mechanisms.
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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