Numerical simulation of acoustic radiation in supersonic mixing layer

MA Liyu; FANG Yihong

doi:10.7638/kqdlxxb-2017.0123

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Numerical simulation of acoustic radiation in supersonic mixing layer

更新时间：2026-05-28

- Numerical simulation of acoustic radiation in supersonic mixing layer
- Vol. 37, Issue 5, Pages: 770-776(2019)
- 作者机构：
  
  天津大学机械工程学院高速空气动力学研究室,天津,300072
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2017.0123
  CLC： V211.3
- Published：2019
- 稿件说明：
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马利宇, 方一红. 超声速混合层气动声场的数值模拟[J]. 空气动力学学报, 2019, 37(5): 770-776.

MA Liyu, FANG Yihong. Numerical simulation of acoustic radiation in supersonic mixing layer[J]. 2019, 37(5): 770-776.
马利宇, 方一红. 超声速混合层气动声场的数值模拟[J]. 空气动力学学报, 2019, 37(5): 770-776. DOI： 10.7638/kqdlxxb-2017.0123.

MA Liyu, FANG Yihong. Numerical simulation of acoustic radiation in supersonic mixing layer[J]. 2019, 37(5): 770-776. DOI： 10.7638/kqdlxxb-2017.0123.

摘要

超声速混合层的噪声是气动声学研究的经典问题，制约着航空发动机性能的提升。本文用数值方法对超声速混合层声辐射特性进行研究，具体方法：用抛物化稳定性方程（PSE）计算混合层近场大尺度扰动演化，结合一种基于渐进展开和稳定性分析的积分预测远场声压，得到快慢两种模态马赫波辐射的强度和方向。分析了上下侧来流温度对气动声场的影响，结果表明，上下侧温度比小于1时，慢模态占优；而上下侧温度比大于1时，快模态占优。

Abstract

The problem of acoustic radiation restricts the performance of aero-engine. To further reveal the acoustic radiation mechanism of mixing layer under supersonic flow

and enhance the understanding

this paper studies the acoustic characteristics of supersonic mixing layer. The near field calculation is investigated by numerical simulation of parabolized stability equations (PSE)

and an integral theory based on stability theory is applied to predict the far field acoustic pressure. The intensity and direction of Mach wave are calculated and in good agreement with previous results. The influence of the flow temperature at the upper and the lower sides is discussed in detail. The results show that

the slow mode dominates when the temperature ratio is less than 1

while the fast mode dominates when the temperature ratio is greater than 1.

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references

LIU J T C. Developing large-scale wavelike eddies and the near jet noise field[J]. Journal of Fluid Mechanics, 1974, 62(3):437-464.

TAM C K W, BURTON D E. Sound generated by instability waves of supersonic flows. Part 1. Two-dimensional mixing layers[J]. Journal of Fluid Mechanics, 1984, 138:249-271.

SONG G, ALIZARD F, ROBINET J C, et al. Global and Koopman modes analysis of sound generation in mixing layers[J]. Physics of Fluids, 2013, 25(12):124101.

ZHONG S Y, HUANG X. A review of aeroacoustics and flow-induced noise for beginners[J]. Acta Aerodynamica Sinica, 2018, 36(3):363-371. (in Chinese)

LI X D, XU X H, GAO J H, et al. Progress and prospect on jet noise study[J]. Acta Aerodynamica Sinica, 2018, 36(3):398-409. (in Chinese)

FREUND J B, LELE S K, MOIN P. Calculation of the radiated sound field using an open Kirchhoff surface[J]. AIAA Journal, 1996, 34(5):909-916.

KANDULA M. Simulation of supersonic jet noise with nonlinear CFD and Kirchhoff surface integral[J]. Engineering Applications of Computational Fluid Mechanics, 2008, 2(4):456-465.

GLOERFELT X, BAILLY C, JUVÉ D. Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods[J]. Journal of Sound Vibration, 2003, 266(1):119-146.

HERBERT T. Parabolized stability equations[J]. Annual Review of Fluid Mechanics, 1997, 29(1):245-283.

PIOT E, CASALIS G, MULLER F, et al. Investigation of the PSE approach for subsonic and supersonic hot jets. Detailed comparisons with LES and linearized Euler equations results[J]. International Journal of Aeroacoustics, 2006, 5(4):361-393.

COLONIUS T, SAMANTA A, GUDMUNDSSON K. Parabolized stability equation models of large-scale jet mixing noise[J]. Procedia Iutam, 2010, (6):64-73.

CHEUNG L, LELE S. Acoustic radiation from subsonic and supersonic mixing layers with nonlinear PSE[C]//42nd AIAA Aerospace Sciences Meeting and Exhibit. 2004: 363.

SINHA A, RODRÍGUEZ D, BRōS G A, et al. Wavepacket models for supersonic jet noise[J]. Journal of Fluid Mechanics, 2014, 742:71-95.

WU X. Mach wave radiation of nonlinearly evolving supersonic instability modes in shear layers[J]. Journal of Fluid Mechanics, 2005, 523:121-159.

ZHANG C Y, FANG Y H. Studing sound generation mechanisms of mixing layer using nonlinear disturbance equations[J]. Acta Aerodynamica Sinica, 2016, 34(5):659-665.

GUO N, FANG Y H. Studying of mach wave radiation in an axisymmetric supersonic jet using nonlinear disturbance equations[J]. Chinese Journal of Computational Mechanics, 2017, 34(2):213-218. (in Chinese)

DAY M J, MANSOUR N N, REYNOLDS W C. Nonlinear stability and structure of compressible reacting mixing layers[J]. Journal of Fluid Mechanics, 2001, 446:375-408.

CHARY P S, SAMANTA A. Linear models for sound from supersonic reacting mixing layers[J]. Physical Review Fluids, 2016, 1(8):083801.

JACKSON T L, GROSCH C E. Inviscid spatial stability of a compressible mixing layer[J]. Journal of Fluid Mechanics, 1989, 208:609-637.

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