超声速燃烧不稳定性研究进展
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摘要
对超声速燃烧不稳定性这一新兴领域的研究进行了综合评述,并对未来研究进行了展望。首先分析了超声速燃烧不稳定性现象的基本特性及其影响因素;随后讨论了超声速燃烧不稳定性的多种机理;接着概括了基于上述机理的超声速燃烧不稳定性建模;最后对超声速燃烧不稳定性还需重点研究的方向给出建议。综述表明,超声速燃烧不稳定性的现象、机理和建模都还需持续开展研究,特别需要关注的是燃烧室构型布局和燃料喷注方式对超燃冲压发动机燃烧不稳定性现象的影响,在超声速混合层和射流等典型流动中更深入探索超声速燃烧不稳定性机理,基于超声速燃烧系统的湍流时空演化特性进一步发展超声速燃烧不稳定性模型。
The present paper conducts a review of the research on the new field "supersonic combustion instability".Firstly,the basic properties and affecting factors of the phenomena of the supersonic combustion instability are analyzed;then,several kinds of mechanisms of the supersonic combustion instability are discussed;thirdly,the modeling of the supersonic combustion instability based on the above mechanisms is summarized;finally,the directions of the supersonic combustion instability that need essential concern are suggested.The review demonstrates that the phenomenon,mechanisms and modeling of the supersonic combustion instability all need continuous researches.The future researches may focus on the effects of the combustion chamber configuration and fueling scheme on the phenomena of the scramjet combustion instability,further explore the mechanisms of the supersonic combustion instability in the canonical flows such as supersonic mixing layers and jets,and further develop models of the supersonic combustion instability based on spatial and temporal evolution of the turbulent characteristics of the supersonic combustion systems.
The present paper conducts a review of the research on the new field "supersonic combustion instability".Firstly,the basic properties and affecting factors of the phenomena of the supersonic combustion instability are analyzed;then,several kinds of mechanisms of the supersonic combustion instability are discussed;thirdly,the modeling of the supersonic combustion instability based on the above mechanisms is summarized;finally,the directions of the supersonic combustion instability that need essential concern are suggested.The review demonstrates that the phenomenon,mechanisms and modeling of the supersonic combustion instability all need continuous researches.The future researches may focus on the effects of the combustion chamber configuration and fueling scheme on the phenomena of the scramjet combustion instability,further explore the mechanisms of the supersonic combustion instability in the canonical flows such as supersonic mixing layers and jets,and further develop models of the supersonic combustion instability based on spatial and temporal evolution of the turbulent characteristics of the supersonic combustion systems.
引文
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[4]Li F,Yu X L,Tong Y G,et al.Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8[J].Aerospace Science and Technology,2013,28(1):72-78.
[5]Sun M B,Zhong Z,Liang J H,et al.Experimental investigation of supersonic model combustor with distributed injection of supercritical kerosene[J].Journal of Propulsion and Power,2014,30(6):1537–1542.
[6]Moule Y,Sabel'Nikov V,Mura A,et al.Computational fluid dynamics investigation of a Mach 12 scramjet engine[J].Journal of Propulsion and Power,2014,30(2):461-473.
[7]Bricalli M G,Brown L M,Boyce R R.Numerical investigation into the combustion behavior of an inlet-fueled thermalcompression-like scramjet[J].AIAA Journal,2015,53(7):1740-1760.
[8]Doherty L J,Smart M K,Mee D J.Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10[J].AIAA Journal,2015,53(11):3196-3207.
[9]Fureby C,Nordin-Bates K,Petterson K,et al.A computational study of supersonic combustion in strut injector and hypermixer flow fields[J].Proceedings of the Combustion Institute,2015,35(2):2127-2135.
[10]Nakaya S,Tsue M,Kono M,et al.Effects of thermally cracked component of n-dodecane on supersonic combustion behaviors in a scramjet model combustor[J].Combustion and Flame,2015,162(10):3847-3853.
[11]Li X P,Liu W D,Pan Y,et al.Investigation on ignition enhancement mechanism in a scramjet combustor with dual cavity[J].Journal of Propulsion and Power,2016,32(2):439-447.
[12]Denman Z J,Chan W Y K,Brieschenk S,et al.Ignition experiments of hydrocarbons in a Mach 8 shape-transitioning scramjet engine[J].Journal of Propulsion and Power,2016,32(6):1462-1471.
[13]Busa K M,Rice B E,Fulton J A,et al.Scramjet Combustion efficiency measurement via tomographic absorption spectroscopy and particle image velocimetry[J].AIAA Journal,2016,54(8):2463-2471.
[14]Cao R F,Cui T,Yu D R,et al.New method for solving onedimensional transonic reacting flows of a scramjet combustor[J].Journal of Propulsion and Power,2016,32(6):1403-1412.
[15]Zhang S K,Li J,Qin F,et al.Numerical investigation of combustion field of hypervelocity scramjet engine[J].Acta Astronautica,2016,129(12):357-366.
[16]Zhu S H,Xu X,Ji P F.Flame stabilization and propagation in dual-mode scramjet with staged-strut injectors[J].AIAA Journal,2017,55(1):171-179.
[17]Baurle R A.Hybrid Reynolds-averaged/large-eddy simulation of a cavity flameholder:modeling sensitivities[J].AIAA Journal,2017,55(2):524-543.
[18]Baurle R A.Hybrid Reynolds-averaged/large-eddy simulation of a scramjet cavity flameholder[J].AIAA Journal,2017,55(2):544-560.
[19]Liu Q L,Baccarella D,Hammack S,et al.Influences of freestream turbulence on flame dynamics in a supersonic combustor[J].AIAA Journal,2017,55(3):913-918.
[20]Bao H,Zhou J,Pan Y.The effect of kerosene injection on ignition probability of local ignition in a scramjet combustor[J].Acta Astronautica,2017,132(3):54-58.
[21]Li X P,Liu W D,Pan Y,et al.Characterization of kerosene distribution around the ignition cavity in a scramjet combustor[J].Acta Astronautica,2017,134(5):11-16.
[22]Abul-Huda Y M,Gamba M.Combustion effects of a staged transverse jet and pulsed detonation in supersonic crossflow[J].Proceedings of the Combustion Institute,2017,36(2):2681-2689.
[23]Miller J D,Peltier S J,Slipchenko M N,et al.Investigation of transient ignition processes in a model scramjet pilot cavity using simultaneous 100 k Hz formaldehyde planar laser-induced fluorescence and chemiluminescence imaging[J].Procee-dings of the Combustion Institute,2017,36(2):2865-2872.
[24]Denman Z J,Wheatley V,Smart M K,et al.Supersonic combustion of hydrocarbons in a shape-transitioning hypersonic engine[J].Proceedings of the Combustion Institute,2017,36(2):2883-2891.
[25]Nordin-Bates K,Fureby C,Karl S,et al.Understanding scramjet combustion using LES of the Hy Shot II combustor[J].Proceedings of the Combustion Institute,2017,36(2):2893-2900.
[26]Gao Z X,Jiang C W,Lee C H.Representative interactive flamelet model and flamelet/progress variable model for supersonic combustion flows[J].Proceedings of the Combustion Institute,2017,36(2):2937-2946.
[27]Bouheraoua L,Domingo P,Ribert G.Large-eddy simulation of a supersonic lifted jet flame:Analysis of the turbulent flame base[J].Combustion and Flame,2017,179(5):199-218.
[28]Deluca L Summerfield M.Nonsteady burning and combustion stability of solid propellants[M].Progress in Astronautics and Aeronautics,Vol.143,Washington D.C.:AIAA,1992.
[29]狄连顺,邢馥源.用挡流板防止火箭发动机燃烧振荡的探讨[J].宇航学报,1986,7(2):72-80.[An approach of preventing combustion vibrations of the rocket engine with lateral baffle[J].Journal of Astronautics,1986,7(2):72-80.]
[30]Yang V,Anderson W E.Liquid rocket engine combustion instability[J].Progress in Astronautics and Aeronautics,Vol.169,1995.
[31]王枫,李龙飞,张贵田.液氧煤油补燃发动机喷注器高频燃烧不稳定性的试验研究[J].宇航学报,2012,33(2):260-264.[Wang Feng,Li Long-fei,Zhang Gui-Tian.Experimental study on high frequency combustion instability with coaxial injector of staged combustion LOX/kerosene rocket engine[J].Journal of Astronautics,2012,33(2):260-264.]
[32]王延涛,薛帅杰,杨岸龙,等.同轴喷嘴自发激励高频燃烧不稳定性试验研究[J].宇航学报,2015,36(12):1414-1420.[Wang Yan-tao,Xue Shuai-Jie,Yang An-long,et al.Experimental investigation for spontaneous high frequency combustion instability of a coaxial injector[J].Journal of Astronautics,2015,36(12):1414-1420.]
[33]Crump J E,Schadow K C,Culick F E,et al.Longitudinal combustion instabilities in ramjet engines:identification of acoustic modes[J].Journal of Propulsion and Power,1986,2:105-109.
[34]Lieuwen T C,Yang V.Combustion instabilities in gas turbine engines:operational experience,fundamental mechanisms,and modeling[M].Progress in Astronautics and Aeronautics,Vol.210,Washington D.C.:AIAA,2005.
[35]李磊,孙晓峰.推进动力系统燃烧不稳定性产生的机理、预测及控制方法[J].推进技术,2010,31(6):710-720.[Li Lei,Sun Xiao-feng.Mechanism,prediction and control method of combustion instability in propulsion system[J].Journal of Propulsion Technology,2010,31(6):710-720.]
[36]Choi J Y,Ma F H,Yang V.Combustion oscillations in a scramjet engine combustor with transverse fuel injection[J].Proceedings of the Combustion Institute,2005,30(2):2851-2858.
[37]Ma F H,Li J,Yang V,et al.Thermoacoustic flow instability in a scramjet combustor.AIAA-2005-3824[R].Reston:AIAA,2005.
[38]Li J,Ma F H,Yang V,et al.A comprehensive study of combustion oscillations in a hydrocarbon-fueled scramjet engine.AIAA-2007-836[R],Reston:AIAA,2007.
[39]Lin K C,Jackson K,Behdadnia R,et al.Acoustic characterization of an ethylene-fueled scramjet combustor with a cavity flameholder[J].Journal of Propulsion and Power,2010,26(6):1161-1169.
[40]Micka D J.Combustion stabilization,structure,and spreading in a laboratory dual-mode scramjet combustor[D].Ann Arbor:The University of Michigan,2010.
[41]Wang H B,Wang Z G,Sun M B,et al.Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder[J].Proceedings of the Combustion Institute,2013,34:2073-2082.
[42]Wang H B,Wang Z G,Sun M B,et al.Nonlinear analysis of combustion oscillations in a cavity-based supersonic combustor[J].Science China Technological Science,2013,56:1093-1101.
[43]Wang H B,Wang Z G,Sun M B.Experimental study of oscillations in a scramjet combustor with cavity flameholders[J].Experimental Thermal and Fluid Science,2013,45:259-263.
[44]Wang H B,Wang Z G,Sun M B,et al.Large-eddy/Reynoldsaveraged Navier-Stokes simulation of combustion oscillations in a cavity-based supersonic combustor[J].International Journal of Hydrogen Energy,2013,38:5918-5927.
[45]Wang Z G,Sun M B,Wang H B,et al.Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor[J].Proceedings of the Combustion Institute,2015,35:2137-2144.
[46]Sun M B,Cui X D,Wang H B,et al.Flame flashback in a supersonic combustor fueled by ethylene with cavity flameholder[J],Journal of Propulsion and Power,2015,31(3):976-980.
[47]Ouyang H,Liu W D,Sun M B.The large-amplitude combustion oscillation in a single-side expansion scramjet combustor[J].Acta Astronautica,2015,117(1):90-98.
[48]Ouyang H,Liu W D,Sun M B.Parametric study of combustion oscillation in a single-side expansion scramjet combustor[J],Acta Astronautica,2016,127(1):603-613.
[49]Ouyang H,Liu W D,Sun M B.The influence of cavity parameters on the combustion oscillation in a single-side expansion scramjet combustor[J],Acta Astronautica,2017,137(1):52-59.
[50]Sun M B.Investigation on the mechanism of the low-frequency combustion instability in unsteady supersonic reacting flows[C].International Symposium on Combustion Instabilities,Beijing,January 05-09,2017.
[51]Tian X D,Chen L H,Gu H B,et al.Experimental study of combustion oscillations in a dual mode scramjet.AIAA-2015-3587[R].Reston:AIAA,2015.
[52]Huang Z W,He G Q,Wang S,et al.Simulations of combustion oscillation and flame dynamics in a strut-based supersonic combustor[J].International Journal of Hydrogen Energy,2017,42(12):8278-8287.
[53]Chen Q,Wang B,Zhang H Q,et al.Numerical investigation of H2/air combustion instability driven by large scale vortex in supersonic mixing layers[J].International Journal of Hydrogen Energy,2016,41(4):3171-3184.
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