亚声速旋拧射流噪声中的温度效应
收稿日期: 2016-03-03
修回日期: 2016-03-24
网络出版日期: 2016-04-05
基金资助
国家自然科学基金(11232011,11402262,11572314);中国博士后科学基金(2014M561833);中央高校基本科研业务费专项资金
Temperature effects on noise in subsonic swirling jets
Received date: 2016-03-03
Revised date: 2016-03-24
Online published: 2016-04-05
Supported by
National Natural Science Foundation of China (11232011, 11402262, 11572314);China Postdoctoral Science Foundation (2014M561833);the Fundamental Research Funds for Central Universities of China
采用大涡模拟(LES)方法模拟亚声速旋拧射流,着重考察温度效应对旋拧射流近场流动演化过程、湍流脉动空间发展和远场噪声的影响。线性稳定性分析表明,旋拧射流中提高射流中心温度会增加剪切层的扰动增长率;数值结果显示,加热会促进剪切层中大尺度结构的产生及相互作用,促使流动更快进入湍流状态,并缩短射流势核区的长度。在初始层流发展阶段,加热会提高中心线上的流向速度脉动峰值,但是对剪切层中的流向速度脉动峰值几乎没有影响;在湍流发展阶段,提高射流中心温度会提高流向速度脉动衰减率,并降低脉动幅值。此外,在非等温射流中,密度脉动幅值要远高于等温射流。在30°方位角附近,等温射流的总声压级幅值最高,冷射流的噪声幅值最低。方位角大于50°时,加热使总声压级降低,且随着方位角幅值的增大,降低越明显;而冷却则会提高总的声压级幅值。
杨海华 , 周林 , 万振华 , 孙德军 . 亚声速旋拧射流噪声中的温度效应[J]. 航空学报, 2016 , 37(8) : 2436 -2444 . DOI: 10.7527/S1000-6893.2016.0100
Large eddy simulation (LES) is performed for investigating temperature effects in subsonic swirling jets. The effects on the flow development and far-field noise are discussed in detail. The results of linear stability theory show that the growth rates of the shear layers are raised as the core temperature increases; the LES results show that heating promotes the interactions of large-scale structures, makes the flows develop into turbulence more quickly and shortens jet potential cores. At the laminar stage, heating raises the peak of axial velocities fluctuations in center lines; however, it has negligible influence on the peak values in shear layers. At the turbulent stage, as the core temperature increases, the levels of velocity fluctuations become lower and the decay rates become higher. Additionally, it is found that the density fluctuations in non-isothermal jets are much higher than those in isothermal jets. At polar angles near 30°, the overall sound pressure level of the hot jet is lower than that in the isothermal jet and higher than that in the cold jet. However, when polar angle is larger than 50°, heating reduces the sound pressure level and the reduction becomes much larger as polar angle increases. While, the sound pressure level increases slightly in the cold jet.
Key words: swirling jet; large eddy simulation; temperature effect; noise; coherent structure
[1] LIGHTHILL M J. On sound generated aerodynamically. I. General theory[J]. Proceedings of the Royal Society A, 1952, 211(1107):564-587.
[2] TAM C K W. Supersonic jet noise[J]. Annual Review of Fluid Mechanics, 1995, 27:17-43.
[3] TAM C K W. Jet noise:Since 1952[J]. Theoretical and Computational Fluid Dynamics, 1998, 10(1):393-405.
[4] RAMAN G. Supersonic jet screech:Half-century from powell to the present[J]. Journal of Sound and Vibration, 1999, 225(3):543-571.
[5] TAM C K W, MORRIS P J. The radiation of sound by the instability waves on a compressible plane turbulent shear layer[J]. Journal of Fluid Mechanics, 1980, 98(5):349-381.
[6] JORDAN P, COLONIUS T. Wave packets and turbulent jet noise[J]. Annual Review Fluid Mechanics, 2013, 45(2):173-195.
[7] MOLLO-CHRISTENSEN E, KOLPIN M A, MARTUCELLI J R. Experiments on jet flows and jet noise far-field spectra and directivity patterns[J]. Journal of Fluid Mechanics, 1964, 18(2):285-301.
[8] TAM C K W, VISWANATHAN K, AHUJA K K, et al. The source of jet noise:Experimental evidence[J]. Journal of Fluid Mechanics, 2008, 615(4):253-292.
[9] VISWANNATHAN K. Analysis of the two similarity components of turbulent mixing noise[J]. AIAA Journal, 2002, 40(9):1735-1744.
[10] VISWANNATHAN K. Aeroacoustics of hot jets[J]. Journal of Fluid Mechanics, 2004, 516(516):39-82.
[11] GUDMUNDSSON K, COLOUNIUS T. Instaiblity wave models for the near-field fluctuations of turbulent jets[J]. Journal of Fluid Mechanics, 2011, 689:97-128.
[12] CAVALIERI A V G, RODRíGUEZ D, JORDAN P, et al. Wavepackets in the velocity field of turbulent jets[J]. Journal of Fluid Mechanics, 2013, 730(5):559-592.
[13] SINHA A, RODRíGUEZ D, BRèS G A, et al. Wavepacket models for supersonic jet noise[J]. Journal of Fluid Mechanics, 2014, 742(742):71-95.
[14] COLONIUS T, LELE S K. Computational aeroacoustics:Progress on nonlinear problems of sound generation[J]. Progress in Aerospace Sciences, 2004, 40(6):345-416.
[15] BOGEY C, BAILLY C, JUVÉ D. Noise investigation of a high subsonic, moderate Reynolds number jet using a compressible large eddy simulation[J]. Theoretical and Computational Fluid Dynamics, 2003, 16(4):273-297.
[16] BODONY D J, LELE S K. On using large eddy simulation for the prediction of noise from cold and heated turbulent jets[J]. Physics of Fluids, 2005, 17(8):119901.
[17] BOGEY C, BAILLY C. An analysis of the correlations between the turbulent flow and the sound pressure fields of subsonic jets[J]. Journal of Fluid Mechanics, 2007, 583(3):71-97.
[18] GOLDSTEIN M E, LEIB S J. The role of instability waves in predicting jet noise[J]. Journal of Fluid Mechanics, 2005, 525:37-72.
[19] TANNA T K. An experimental study of jet noise PartⅠ:Turbulent mixing noise[J]. Journal of Sound and Vibration, 1977, 50(3):405-428.
[20] WAN Z H, ZHOU L, YANG H H, et al. Large eddy simulation of flow development and noise generation of free and swirling jets[J]. Physics of Fluids, 2013, 25(12):126103-1-27.
[21] FREUND J B. Noise sources in a low-Reynolds-number jet at Mach 0.9[J]. Journal of Fluid Mechanics, 2001, 438(5):277-305.
[22] STROMBERG J L, MCLAUGHLIN D K, TROUT T R. Flow field and acoustic properties of a Mach number 0.9 jet at a low Reynolds number[J]. Journal of Sound and Vibration, 1980, 72(2):159-176.
[23] KEIDERLING F, KLEISER L, BOGEY C. Numerical study of eigenmode forcing effects on jet flow development and noise generation mechanisms[J]. Physics of Fluids, 2009, 21(4):119-135.
[24] BROWN G L, ROSHKO A. On density effect and large structure in turbulent mixing layers[J]. Journal of Fluid Mechanics, 1974, 64(4):775-816.
[25] CROW S C, CHAMPAGNE F H. Orderly structure in jet turbulence[J]. Journal of Fluid Mechanics, 1971, 48(3):547-591.
[26] LAU J C, MORRIS P J, FISHER, M J. Measurements in subsonic and supersonic free jets using a laser velocimeter[J]. Journal of Fluid Mechanics, 1979, 93(1):1-27.
[27] RAMAN G, RICE E J, RESHOTKO E. Mode spectra of natural disturbances in a circular jet and the effects of acoustic forcing[J]. Experiments in Fluids, 1994, 17(6):415-426.
[28] BOGEY C, BAILLY C. Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets[J]. Journal of Fluid Mechanics, 2010, 663(11):507-538.
[29] BOGEY C, MARSDEN O, BAILLY C. Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of 105[J]. Journal of Fluid Mechanics, 2012, 701(6):352-385.
[30] ZAMAN K B M Q. Flow field and near and far sound field of a subsonic jet[J]. Journal of Sound and Vibration, 1986, 106(1):1-16.
[31] AHUJA K K, LEPICOVSKY J, TAM C K W, et al. Tone excited jet-theory and experiment:NASA-CR-3538[R]. Washington, D.C.:NASA, 1982.
[32] BOGEY C, BAILLY C. Investigation of downstream and sideline subsonic jet noise using large eddy simulation[J]. Theoretical Computational Fluid Dynamics, 2006, 20(1):23-40.
[33] LUSH P A. Measurements of subsonic jet noise and comparison with theory[J]. Journal of Fluid Mechanics, 1971, 46(3):477-500.
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