流体力学、飞行力学与发动机

基于Kirchhoff方法亚声速平面混合层主涡对并声场分析

  • 冯峰 王强
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  • 中国航天空气动力技术研究院

收稿日期: 2012-04-16

  修回日期: 2012-06-03

  网络出版日期: 2012-06-18

Analysis of Acoustic Field of Primary Vortex Pairing in Subsonic Plane Mixing Layers Using Kirchhoff Method(N0.12-15995)

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Received date: 2012-04-16

  Revised date: 2012-06-03

  Online published: 2012-06-18

摘要

为拓展主涡对并气动声场计算分析方法研究,针对亚声速平面混合层主涡对并流动,采用直接数值模拟方法求解获取近场声源,利用二维Kirchhoff频域法和时域法外推声辐射远场,并应用Kirchhoff频域法对主涡二次对并声辐射特征进行分析。研究结果表明Kirchhoff频域法和时域法具有一定差异性,但与主涡对并直接声计算结果对比,显示二者计算精度相当且均具有较高的精确性。通过Kirchhoff频域法应用分析,清晰揭示出主涡二次对并各声模态与主涡卷起、对并过程的对应相关性,利用频域法这种良好的计算分析性能,本文进一步研究了混合层入口扰动相位差对涡并声场的影响,展现出主导声波在声场中的重要作用。

本文引用格式

冯峰 王强 . 基于Kirchhoff方法亚声速平面混合层主涡对并声场分析[J]. 航空学报, 0 , 0(0) : 0 -0 . DOI: 10.7527/S1000-6893.2013.0082

Abstract

In order to expand the calculation and analysis method research of acoustic ?eld generated by vortex pairing, the subsonic planar mixing layer vortex pairing is studied with numerical method. Direct numerical simulation (DNS) is employed to extract the acoustic source, the two dimensional frequency domain and time domain Kirchhoff methods are applied to extrapolate the far-field radiated sound, and the frequency domain method is employed to investigate the sound radiation from the twice vortex pairings. The frequency domain and time domain Kirchhoff methods are different in some degree, but the computation results compared with the DNS show that they reach the similar high order of accuracy. According to the analysis with frequency domain Kirchhoff method, it reveal clearly that each acoustic mode of the twice vortex pairings correspond to the vortex rolls and pairings respectively. Using the fre-quency domain method’s good performance of computational and analytica, this paper farther studies the influence of inflow instability waves with different phases on the acoustic field of vortex pairings, and exhibits that the dominant mode plays an important role in the acoustic field.

参考文献

Suzuki T, Lele S K. Acoustic scattering from a mixing layer: role of instability waves [R]. AIAA Paper 1999- 0228, 1999.
[2] Colonius T, Lele S K, Moin P. Sound generation in a mixing layer [J]. Journal of Fluid Mechanics, 1997, 330: 375-409.
[3] Bogey C, Bailly C, Juvé D. Numerical simulation of sound generated by vortex pairing in a mixing layer [J]. AIAA Journal, 2000, 38(12): 2210-2218.
[4] Farassat F, Doty M J, Hunter C A. The acoustic analogy - a powerful tool in aeroacoustics with emphasis on jet noise prediction [R]. AIAA Paper 2004-2872, 2004.
[5] Lyrintzis A S, Pilon A, Meadows K. The use of Kirchhoff's method in jet aeroacoustics [R]. NASA-TM- 112990, 1995.
[6] Cheung L C, Lele S K. Acousitc radiation from subsonic and supersonic mixing layers with nonlinear PSE [R]. AIAA Paper 2004-0363, 2004.
[7] Tam C K W, Dong Z. Radiation and outflow boundary conditions for direct computation of acoustic and flow disturbances in a nonuniform mean flow [J]. Journal of Sound and Vibration, 1996, 4(2): 175-201.
[8] 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 and Vibration, 2003, 266: 119-146.
[9] Lockard D P. An efficient, two-dimensional implementation of the Ffowcs Williams and Hawkings equation [J]. Journal of Sound and Vibration, 2000, 229(4): 897–911.
[10] Guo Y P. Application of the Ffowcs Williams-Hawkings equation to two-dimensional problems [J]. Journal of Fluid Mechanics, 2000, 403: 201-221.
[11] Tam C K W, Webb J C. Dispersion-relation-preserving finite difference schemes for computational acoustics [J]. Journal of Computational Physics, 1993, 107(2): 262-281.
[12] Berland J, Bogey C, Bailly C. Optimized explicit schemes: matching and boundary schemes and 4th-order Runge-Kutta algorithm [R]. AIAA Paper 2004-2814, 2004.
[13] 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.
[14] Eldredge J D. The acoustics of two-dimensional leapfrogging vortices [R]. AIAA Paper 2005-2954, 2005.
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