液体射流喷入横向气流混合特性研究进展

doi:10.7527/S1000-6893.2013.0346

Abstract

Abstract:

Attention is now focused on the spray mixing characteristics of liquid jet injected into subsonic air crossflows as a development of low emission combustion technology. This paper summarizes the research progress in this field. The review is mainly about the experimental research work carried out at home and abroad, from three aspects: the atomization and breakup of a liquid jet in a crossflow, liquid jet penetration in the crossflow, and spray dispersion and transport in the crossflow. In most studies a liquid jet from a single plain orifice is transversely injected into a uniform airflow. The influences of fuel pulsation, shear layer and swirl in the airflow on spray mixing characteristics are studied experimentally. However, few studies are carried out on the mixing of an airblast-atomized liquid spray or multiple liquid jet injected into a crossflow. Finally a brief summary is given of the experimental studies on the spray mixing characteristics of a liquid jet injected into a crossflow. According to the review of the progress on the mixing characteristics of liquid jet, further research work is proposed by this paper with the application on atomization in advanced low emission combustors as the background.

Key words: liquid jet, crossflow, mixing, breakup, penetration height, low emission

CLC Number:

V231.2

LIN Yuzhen, LI Lin, ZHANG Chi, XU Huasheng. Progress on the Mixing of Liquid Jet Injected Into a Crossflow[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(1): 46-57.

References

[1] Hojnacki J T. Ramjet engine fuel injection studies: DTIC document[R]. AD0754852, 1972.

[2] Wotel G J, Gallagher K E, Caron S D, et al. High speed turbo ramjet combustor technology program, Volume 1: Final Report, WL-TR-91-2043[R]. 1991.

[3] Yates C L. Liquid injection into a supersonic stream: DTIC document, AD0741887[R]. 1972.

[4] Lefebvre A H, Ballal D R, Bahr D W. Gas turbine combustion: alternative fuels and emissions[M]. Boca Raton, FL: CRC Press, 2010.

[5] Lin Y Z, Xu Q H, Liu G E. Gas turbine combustor[M]. Beijing: National Defense Industry Press, 2008. (in Chinese) 林宇震, 许全宏, 刘高恩. 燃气轮机燃烧室[M]. 北京: 国防工业出版社, 2008.

[6] Foust M J, Thomsen D, Stickles R, et al. Development of the GE aviation low emissions TAPS combustorfor next generation aircraft engines[C]//Proceedings of the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012.

[7] Lazik W, Doerr Th, Bake S, et al. Development of lean-burn low-NO_x combustion technology at rolls-royce deutschland[C]//Proceedings of the ASME Turbo Expo, 2008, 3(PART): 797-807.

[8] Fric T F. Effects of fuel-air unmixedness on NO(x) emissions[J]. Journal of Propulsion and Power, 1995, 9(5): 708-713.

[9] Lyons V J. Fuel/air nonuniformity-effect on nitric oxide emissions[C]//Proceedings of the 19th Aerospace Sciences Meeting, 1981.

[10] Mello J P, Mellor A M, Steele R C, et al. A study of the factors affecting NO(x) emissions in lean premixed turbine combustors[C]//Proceedings of the 33rd Joint Propulsion Conference and Exhibit, 1997.

[11] Barnes J C, Mellor A M. Effects of unmixedness in piloted-lean premixed gas-turbine combustors[J]. Journal of Propulsion and Power, 1998, 14(6): 967-973.

[12] Mello J P, Mellor A M. Modeling NO(x) emissions from lean-premixed turbine combustors with swirling, non-uniform fuel/air mixtures[C]//Proceedings of the 35th Joint Propulsion Conference and Exhibit, 1999.

[13] Frazier T R, Foglesong R E, Coverdill R E, et al. An experimental investigation of fuel/air mixing in an optically accessible axial premixer[C]//Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998.

[14] Lefebvre A H. Atomization and sprays[M]. NewYork: Hemisphere Press, 1989.

[15] Gan X H. Aero gas turbine engine fuel nozzle technology[M]. Beijing: National Defense Industry Press, 2006. (in Chinese) 甘晓华. 航空燃气轮机燃油喷嘴技术[M]. 北京: 国防工业出版社, 2006.

[16] Wu P K, Kirkendall K A, Fuller R P, et al. Breakup processes of liquid jets in subsonic crossflows[J]. Journal of Propulsion and Power, 1997, 13(1): 64-73.

[17] Huang Y, Lin Y Z, Fan W J, et al. Combustion and combustor[M]. Beijing: Beihang University Press, 2009. (in Chinese) 黄勇, 林宇震, 樊未军, 等. 燃烧与燃烧室[M]. 北京: 北京航空航天大学出版社, 2009.

[18] Less D M, Schetz J A. Transient behavior of liquid jets injected normal to a high-velocity gas stream[J]. AIAA Journal, 1986, 24(12): 1979-1986.

[19] Inamura T, Nagai N, Watanabe T, et al. Disintegration of liquid and slurry jets traversing subsonic air streams[C]//Proceedings of the Experimental Heat Transfer, Fluid Mechanics, and Thermodynamics, 1993.

[20] Mazallon J, Dai Z, Faeth G. Aerodynamic primary breakup at the surface of nonturbulent round liquid jets in crossflow[C]//Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998.

[21] Sallam K A, Aalburg C, Faeth G M. Primary breakup of round nonturbulent liquid jets in gaseous crossflows[C]//Proceedings of the 41st Aerospace Sciences Meeting and Exhibit, 2003.

[22] Birouk M, Azzopardi B J, Stäbler T. Primary break-up of a viscous liquid jet in a cross airflow[J]. Particle & Particle Systems Characterization, 2003, 20(4): 283-289.

[23] Lubarsky E, Shcherbik D, Bibik O, et al. Fuel jet in cross flow[C]//Experimental study of spray characteristics.Proceedings of the 23rd Annual Conference on Liquid Atomization and Spray Systems (ILASS Americas), 2011.

[24] Gopala Y, Lubarsky E, Zinn B T. Liquid jet in crossflow-a novel method to locate the column breakup point[C]//Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008.

[25] Lakhamraju R R. Liquid jet breakup studies in subsonic airstream at elevated temperatures. Cincinnati, OH: Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, 2005.

[26] Bellofiore A. Experimental and numerical study of liquid jets injected in high-density air crossflow. Naples: Università degli Studi di Napoli Federico Ⅱ, 2007.

[27] Wang Q, Mondragon U M, Brown C T, et al. Characterization of trajectory, break point, and break point dynamics of a plain liquid jet in a crossflow[J]. Atomization and Sprays, 2011, 21(3): 203-219.

[28] Lee K, Aalburg C, Diez F J, et al. Primary breakup of turbulent round liquid jets in uniform crossflows[J]. AIAA Journal, 2007, 45(8): 1907-1916.

[29] Sallam K A, Ng C, Sankarakrishnan R, et al. Breakup of turbulent and non-turbulent liquid jets in gaseous crossflows[C]//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.

[30] Anu O, Khaled S. Effect of nozzle length/diameter ratio on the breakup of round liquid jets in crossflow[C]//Proceedings of the 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008.

[31] Osta A R, Sallam K A. Nozzle-geometry effects on upwind-surface properties of turbulent liquid jets in gaseous crossflow[J]. Journal of Propulsion and Power, 2010, 26(5): 936-946.

[32] Reiche J R, Gopala Y, Lubarsky O, et al. Liquid fuel jet in crossflow-comparison between sharp edged and smooth injection orifice[C]//Proceedings of the 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007.

[33] Fuller R P, Wu P, Kirkendall K A, et al. Effects of injection angle on the breakup processes of liquid jets in subsonic crossflows[C]//Proceedings of the 33rd Joint Propulsion Conference and Exhibit, 1997.

[34] Costa M, Melo M J, Sousa M, et al. Spray characteristics of angled liquid injection into subsonic crossflows[J]. AIAA Journal, 1997, 44(3): 646-653.

[35] Chigier N, Farago Z. Morphological classification of disintegration of round liquid jets in a coaxial air stream[J]. Atomization and Sprays, 1992, 2(2): 137-153.

[36] Leong M I, Vincent G M, Scott G S. Mixing of anairblast-atomized fuel spray injected into a crossflow of air, NASA/CR-2000-210467[R]. 2000.

[37] Zhu Y, Huang Y, Wang F, et al. Experiment on the breakup of round liquid jets in cross airflows[J]. Journal of Aerospace Power, 2010, 25(10): 2261-2266. (in Chinese) 朱英, 黄勇, 王方, 等. 横向气流中的液体圆形射流破碎实验[J]. 航空动力学报, 2010, 25(10): 2261-2266.

[38] Zhu Y, Huang Y, Wang F, et al. Experiment on breakup processes and surface waves of round liquidjets in crossflows[C]//Proceedings of ASME Turbo Expo, 2010.

[39] Wang X H, Huang Y, Wang F, et al. Bag breakup of round liquid jets in crossflow[J]. Journal of Aerospace Power, 2012, 27(9): 1979-1987. (in Chinese) 王雄辉, 黄勇, 王方, 等. 横向气流中液体圆柱射流的破碎特性和表面波现象[J]. 航空动力学报, 2012, 27(9): 1979-1987.

[40] Wang S L, Huang Y, Wang F, et al. On the breakup process of round liquid jets in gaseous crossflows at low Weber number[C]//Proceedings of ASME Turbo Expo, 2013.

[41] Xu S L, Archer R D, Milton B E, et al. Experimental investigation on unsteady transverse injection of kerosene into a supersonic flow[J]. Acta Aerodynamica Sinica, 2000, 18(3): 272-279. (in Chinese) 徐胜利, Archer R D, Milton B E, 等. 煤油在超声速气流中非定常横向喷射的实验观察[J]. 空气动力学学报, 2000, 18(3): 272-279.

[42] Xu S L, Archer R D, Milton B E, et al. Realization of transverse injection of kerosene into a supersonic flow[J]. Science in China (Series E), 2000, 30(2): 179-186. (in Chinese) 徐胜利, Archer R D, Milton B E, 等. 煤油在超声速气流中横向喷射的实现[J]. 中国科学(E辑), 2000, 30(2): 179-186.

[43] Xu S L, Archer R D, Milton B E, et al. Unsteady transverse injection of kerosene into a supersonic flow[J]. Science in China Series E:Technological Sciences, 2000, (2): 206-214.

[44] Xu S L, Yue P T, Archer R D, et al. Experimental study on the unsteady transverse injection of diesel into a subsonic and supersonic flow[J]. Journal of Combustion Science and Technology, 2000, 6(2): 101-106. (in Chinese) 徐胜利, 岳朋涛, Archer R D, 等. 柴油在亚、超声速气流中横向喷射实验研究[J]. 燃烧科学与技术, 2000, 6(2): 101-106.

[45] Xu S L, Yue P T, Sun Y Y, et al. Three dimensional numerical simulation of atomized fuels injected into a supersonic flow[J]. Chinese Journal of Applied Mechanics, 2000, 17(2): 19-23. (in Chinese) 徐胜利, 岳朋涛, 孙英英, 等. 超声速气流中雾化燃料喷射的三维数值研究[J]. 应用力学学报, 2000, 17(2): 19-23.

[46] Liu J. Numerical and experimental investigation of fuel spray in supersonic cross flow[D]. Beijing: School of Astronautics, Beihang University, 2010. (in Chinese) 刘静. 超声速气流中横向燃油喷雾的数值模拟和实验研究[D]. 北京:北京航空航天大学宇航学院, 2010.

[47] Liu J, Wang L, Zhang J, et al. Experimental and numerical simulation of atomization of liquid jet in supersonic cross flow[J]. Journal of Aerospace Power, 2008, 23(4): 724-729. (in Chinese) 刘静, 王辽, 张佳, 等. 超声速气流中横向射流雾化实验和数值模拟[J]. 航空动力学报, 2008, 23(4): 724-729.

[48] Liu J, Xu X. The research development of liquid jet atomization in high speed cross flow[J]. Advances in Mechanics, 2009, 39(3): 273-283. (in Chinese) 刘静, 徐旭. 高速气流中横向液体射流雾化研究进展[J]. 力学进展, 2009, 39(3): 273-283.

[49] Hinze J. Fundamentals of the hydrodynamic mechanism of splitting in dispersion processes[J]. AIChE Journal, 1955, 1(3): 289-295.

[50] Krzeczkowski S A. Measurement of liquid droplet disintegration mechanisms[J]. International Journal of Multiphase Flow, 1980, 6(3): 227-239.

[51] Samuelsen G, Eastes T. Secondary atomization by high amplitude pressure waves[C]//Proceedings of the 28th Joint Propulsion Conference and Exhibit, 1992.

[52] Park S W, Kim S, Lee C S. Breakup and atomization characteristics of mono-dispersed diesel droplets in a cross-flow air stream[J]. International Journal of Multiphase Flow, 2006, 32(7): 807-822.

[53] Wang X H, Huang Y, Wang F, et al. Bag breakup of round liquid jets in crossflow[J]. Journal of Propulsion Technology, 2012, 33(2): 198-204. (in Chinese) 王雄辉, 黄勇, 王方, 等. 横向气流中液体射流袋式破碎机理[J]. 推进技术, 2012, 33(2): 198-204.

[54] Wang X H, Huang Y, Wang S L, et al. Bag breakup of turbulent liquid jets in crossflows[J]. AIAA Journal, 2012, 50(6): 1360-1366.

[55] Elshamy O M. Experimental investigations of steady and dynamic behavior of transverse liquid jets[D]. Cincinnati, OH: Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, 2007.

[56] Gopala Y, Zhang P, Bibik O, et al. Liquid fuel jet in crossflow-trajectory correlations based on the column breakup point[C]//Proceedings of the 48th AIAA Aerospace Sciences Meeting including the New Horizons Forumand Aerospace Exposition, 2010.

[57] Stenzler J N, Lee J G, Santavicca D A, et al. Penetration of liquid jets in a crossflow[C]//Proceedings of the 41st Aerospace Sciences Meeting and Exhibit, 2003.

[58] Li L, Lin Y Z, Xue X, et al. Injection of liquid kerosene into a high-pressure subsonic air crossflow from normal temperature to elevated temperature[C]//Proceedings of the ASME Turbo Expo, 2012.

[59] Xue X, Gao W, Xu Q H, et al. Injection of subcritical and supercritical aviation kerosene into a high-temperature and high-pressure crossflow[C]//Proceedings of the ASME Turbo Expo, 2011.

[60] Soo-Young N. Empirical correlations for penetration height of liquid jet in cross flow-a review[C]//Proceedings of the 24th Annual Conference on Liquid Atomization and Spray Systems, 2011.

[61] Wu P K, Kirkendall K A, Fuller R P, et al. Breakup processes of liquid jets in subsonic crossflows[C]//Proceedings of the 32nd Joint Propulsion Conference and Exhibit, 1996.

[62] Wu P K, Kirkendall K A, Fuller R P, et al. Spray structures of liquid fuel jets atomized in subsonic crossflows[C]//Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998.

[63] Ragucci R, Bellofiore A, Cavaliere A. Breakup and breakdown of bent kerosene jets in gas turbine conditions[J]. Proceedings of the Combustion Institute, 2007, 31(2): 2231-2238.

[64] Yong Seok H, Yu In J. The penetration characteristics of normally injected kerosene liquid jet in high Weber number flow[C]//Proceedings of the 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2009.

[65] Chen T H, Smith C R, Schommer D G, et al.Multi-zone behavior of transverse liquid jet in high-speed flow[C]//Proceedings of the 31st AIAA Aerospace Sciences Meeting and Exhibit, 1993.

[66] Masuda B J, McDonell V G. Penetration of a recessed distillate liquid jet into a crossflow at elevated pressure and temperature[C]//Proceedings of 10th International Conference on Liquid Atomization and Spray System, 2006.

[67] Birouk M, Iyogun C O, Popplewell N. Role of viscosity on trajectory of liquid jets in a cross-airflow[J]. Atomization and Sprays, 2007, 17(3): 267-287.

[68] Bellofiore A, Cavaliere A, Ragucci R. Air density effect on the atomization of liquid jets in crossflow[J]. Combustion Science and Technology, 2007, 179(1-2): 319-342.

[69] Amighi A, Eslamian M, Ashgriz N. Trajectory of a liquid jet in high pressure and high temperature subsonic air crossflow[C]//Proceedings of the ICLASS, 2009.

[70] Tambe S B, Jeng S, Mongia H, et al. Liquid jets in subsonic crossflow[C]//Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit, 2005.

[71] Lakhamraju R R, Jeng S M. Liquid jet breakup studies in subsonic air stream at elevated temperatures[C]//Proceedings of the 18th Annual Conference on Liquid Atomization and Spray Systems (ILASS Americas), 2005.

[72] Yoon H J, Hong J G, Lee C. Correlations for penetration height of single and double liquid jets in cross flow under high-temperature conditions[J]. Atomization and Sprays, 2011, 21(8): 673-686.

[73] Bunce K, Lee J G, Santavicca D A. Characterization of liquid jets-in-crossflow under high temperature, high velocity non-oscillating and oscillating flow conditions[C]//Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.

[74] Elshamy O M, Tambe S B, Cai J, et al. Excited liquid jets in subsonic crossflow[C]//Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007.

[75] Lee I C, Kang Y S, Moon H J, et al. Spray jet penetration and distribution of modulated liquid jetsin subsonic cross-flows[J]. Journal of Mechanical Science and Technology, 2010, 24(7): 1425-1431.

[76] Tambe S, Elshamy O, Jeng S. Liquid jets injected transversely into a shear layer[C]//Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007.

[77] Tambe S B. Liquid jets injected into non-uniform crossflow. Cincinnati, OH: Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, 2010.

[78] Ghosh S, Hunt J C R. Spray jets in a cross-flow[J]. Journal of Fluid Mechanics, 1998, 365(1): 109-136.

[79] Leong M Y, McDonell V G, Samuelsen G S. Effect of ambient pressure on an airblast spray injected into a crossflow[J]. Journal of Propulsion and Power, 2001, 17(5): 1076-1084.

[80] Lee I, Kang Y S, Koo J. Mixing characteristics of pulsed air-assist liquid jet into an internal subsonic cross-flow[J]. Journal of Thermal Science, 2010, 19(2): 136-140.

[81] Oda T, Hiroyasu H, Arai M, et al. Characterization of liquid jet atomization across a high-speed airstream[J]. JSME International Journal Series B, Fluids and Thermal Engineering, 1994, 37(4): 937-944.

[82] Inamura T, Nagai N. Spray characteristics of liquid jet traversing subsonic airstreams[J]. Journal of Propulsion and Power, 1997, 13(2): 250-256.

[83] Kihm K D, Lyn G, Son S. Atomization of cross-injecting sprays into convective air stream[J]. Atomization and Sprays, 1995, 5(4): 417-434.

[84] Lubarsky E, Reichel J R, Zinn B T, et al. Spray in crossflow: dependence on Weber number[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132(2): 021501-1-9.

[85] Leong M, McDonell V, Samuelsen G. Effect of ambient pressure on an airblast spray injected into a crossflow[C]//Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998.

[86] Becker J, Hassa C. Liquid fuel placement and mixing of generic aeroengine premix module at different operating conditions[J]. Journal of Engineering for Gas Turbines and Power, 2003, 125(4): 901-908.

[87] Becker J, Heitz D, Hassa C. Spray dispersion in acounter-swirling double-annular air flow at gas turbine conditions[J]. Atomization and Sprays, 2004, 14(1): 15-35.

[88] Masuda B J, McDonell V G, Oskam G W. Mixing of a plain jet into a swirling crossflow[C]//Proceedings of the 21st Annual Conference on Liquid Atomization and Spray Systems (ILASS Americas), 2008.

[89] Tambe S B, Jeng S M. A study of liquid jets injected transversely into a swirling crossflow[C]//Proceedings of 21st Annual Conference on Liquid Atomization and Spray Systems (ILASS Americas), 2008.

[90] Tambe S B, Jeng S M. Three-dimensional penetration and velocity distribution of liquid jets injected transversely into a swirling crossflow[C]//Proceedings of the 22nd Annual Conference on Liquid Atomization and Spray Systems (ILASS Americas), 2010.

[91] Yang M L, Gu S J, Li X Y. Study on two-phase fuel distributions in high-speed hot transverse air stream[J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(3): 485-490.

[92] Yang M L, Gu S J, Liu G E, et al. Trajectory with diffusion method for predicting the fuel distribution in a transverse stream[C]//Proceedings of the 21st Aerospace Sciences Meeting, 1983.

[93] Zhang H B, Liu L, Sun H J, et al. Study on single-nozzle spray pattern in crossflow and two-phase mixing characteristics[J]. Journal of Xi’an Jiaotong University, 2010, 44(7): 104-108. (in Chinese) 张海滨, 刘利, 孙慧娟, 等. 横流中单喷嘴雾化形态与两相掺混特性研究[J]. 西安交通大学学报, 2010, 44(7): 104-108.

[94] Bai B F, Zhang H B, Liu L, et al. Experimental study on turbulent mixing of spray droplets in crossflow[J]. Experimental Thermal and Fluid Science, 2009, 33(6): 1012-1020.

Progress on the Mixing of Liquid Jet Injected Into a Crossflow

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