Sound generated by axisymmetric non-plane entropy waves passing through flow contractions

IF 1.2 4区 工程技术 Q3 ACOUSTICS International Journal of Aeroacoustics Pub Date : 2022-06-22 DOI:10.1177/1475472X221107368
Dong Yang, Juan Guzmán-Iñigo, A. Morgans
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引用次数: 2

Abstract

For a single-component perfect gas, entropy perturbations are associated with the difference between the overall density fluctuation and that coming from the acoustic perturbation. Entropy perturbations can generate sound when accelerated/decelerated by a non-uniform flow and this is highly relevant to thermoacoustic instabilities for gas turbines and rocket engines, and to noise emission for aero-engines. Widely used theories to model this entropy-generated sound rely on quasi-1D assumptions for which questions of validity were raised recently from both numerical and experimental studies. In the present work, we build upon an acoustic analogy theory for this problem. This theory was initiated by Morfey (J. Sound Vib. 1973) and Ffowcs Williams and Howe (J. Fluid Mech. 1975) about 50 years ago and extended recently by Yang, Guzmán-Iñigo and Morgans (J. Fluid Mech. 2020) to study the effect of non-plane entropy waves at the inlet of a flow contraction on its sound generation. Comparisons against both numerical simulations and previous theory are performed to validate the results.
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轴对称的非平面熵波通过流动收缩时产生的声音
对于单组分理想气体,熵扰动与总密度波动与声学扰动之间的差异有关。熵扰动在被非均匀流加速/减速时会产生声音,这与燃气轮机和火箭发动机的热声不稳定性以及航空发动机的噪声排放高度相关。对这种熵产生的声音进行建模的广泛使用的理论依赖于准一维假设,最近数值和实验研究都提出了这些假设的有效性问题。在目前的工作中,我们建立在声学类比理论的基础上解决这个问题。这一理论由Morfey(J.Sound Vib.1973)和Ffowcs-Williams和Howe(J.Fluid Mech.1975)在大约50年前提出,最近由Yang、Guzmán-Iñigo和Morgans(J.FluidMech.2020)扩展,以研究流动收缩入口处的非平面熵波对其声音产生的影响。对数值模拟和先前理论进行了比较,以验证结果。
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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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