低温液体火箭燃烧室内射流雾化研究进展

丁月; 鲍松龄; 禹云星; 高鑫鑫; 谢军龙; 陈建业

doi:10.13224/j.cnki.jasp.20210181

低温液体火箭燃烧室内射流雾化研究进展

doi: 10.13224/j.cnki.jasp.20210181

华中科技大学能源与动力工程学院，武汉 430074

基金项目: 国家自然科学基金（51806069）

详细信息

作者简介:
丁月（1998-），女，硕士生，主要从事射流雾化方面研究。

通讯作者:
陈建业（1989-），男，讲师、硕士生导师，博士，主要从事低温气液两相流研究。E-mail：jianye_chen@hust.edu.cn

中图分类号: V211
计量
- 文章访问数: 55
- HTML浏览量: 0
- PDF量: 82
- 被引次数: 0
出版历程
- 收稿日期: 2021-04-20
- 刊出日期: 2022-04-28

Recent advances on jet atomization in cryogenic liquid rocket combustion chamber

School of Energy and Power Engineering，Huazhong University of Science and Technology，Wuhan 430074，China

摘要

摘要: 从理论、实验和数值计算方面，阐述和总结了低温推进剂射流雾化的研究现状和进展。对射流雾化机理及形态进行了分类，重点从对比常温流体与低温流体射流雾化特征参数不同的角度，梳理了射流雾化方面的数值研究方法，并介绍了低温射流雾化的相关实验研究。结果表明：空气扰动破碎机理仍是最广为接受的理论，而超临界工况下射流雾化形态不符合现有的射流雾化分类；数值计算方法逐渐由流体体积法和水平集法向直接数值模拟转变，对闪蒸现象的建模是研究重难点之一；低温流体射流喷雾实验数据匮乏，需通过丰富测量手段，提高测量精度的途径获得完整、准确的实验数据。
- 火箭发动机 /
- 燃烧室 /
- 低温推进剂 /
- 射流 /
- 雾化
Abstract: From aspects of theory，experiments and numerical simulation，the research status and progress of cryogenic propellant jet atomization were analyzed and summarized.The mechanism and patterns of jet atomization were classified，the numerical research methods of jet atomization were sorted out and relevant experimental study of cryogenic jet atomization was introduced by comparing different atomization parameters between ambient fluids and cryogenic fluids.It indicates that the air disturbance induced breakup mechanism is the most accepted theory，whereas，the jet atomization morphology under supercritical conditions does not accord with the existing classification.Numerical methods for jet atomization gradually change from the volume of fluid method and level-set method to the direct numerical simulation.Modeling of flashing phenomenon is one of the key points in the simulation.Furthermore，there lacks of experimental data of the cryogenic jet atomization.Enriching measurement methods and improving measurement accuracy can solve this problem.
- rocket engine /
- combustion chamber /
- cryogenic propellant /
- jet /
- atomization

HTML

参考文献(68)

[1]	丁群.基于OpenFOAM的VOF-DDM模型对雾化现象的研究[D].哈尔滨：哈尔滨工程大学，2018.
[2]	HAESELER D,HAIDN O J.Mapping of aluminum particle dispersion in solid rocket fuel formulations[M].Berlin:Springer,2017:427-462.
[3]	LEBAS R,MENARD T,BEAU P A,et al.Numerical simulation of primary break-up and atomization:DNS and modelling study[J].International Journal of Multiphase Flow,2009,35（3）:247-260.
[4]	CHEN Jianye,GAO Xinxin,BAO Songling,et al.Numerical analysis of spray characteristics with liquid nitrogen[J].Cryogenics,2020,109:103-113.
[5]	刘玉强.喷嘴喷雾特性检测技术[J].广东化工,2010,37（11）:253-254.
[6]	REITZ R D,BRACCO F V.Mechanism of atomization of a liquid jet[J].Physics of Fluids,1998,25（10）:1730-1742.
[7]	LIU Huimin.Science and engineering of droplets:fundamentals and applications[J].Applied Mechanics Reviews,1999,55（1）:451-507.
[8]	MIESSE C C.Correlation of experimental data on the disintegration of liquid jets[J].Industrial and Engineering Chemistry,1955,47（9）:1690-1701.
[9]	李霄月.液体射流首次破碎的直接数值模拟研究[D].杭州：浙江大学，2019.
[10]	MENG L,HAIDN O J.Characterization of flashing phenomena with cryogenic fluid under vacuum conditions[J].Journal of Propulsion and Power,2016,32（5）:1253-1263.
[11]	MENG L.Experimental and numerical study of cryogenic flashing spray in spacecraft application[D].München,Germany:Technische Universit?t München,2018.
[12]	ZENG Y B,LEE,CHIA F F.An atomization model for flash boiling sprays[J].Combustion Science and Technology,2001,169（1）:45-67.
[13]	ZHANG Peiyu,WANG Bing.Effects of elevated ambient pressure on the disintegration of impinged sheets[J].Physics of Fluids,2017,29（4）:92-102.
[14]	WEBER C.On the disintegration of a liquid jet[J].Journal of Applied Mathematics and Mechanics,1931,2（11）:136-154.
[15]	RAYLEIGH L.On the instability of jets[J].Proceedings of the London Mathematical Society,1878,1 （1）:4-13.
[16]	TAYLOR F.Instability of liquid jets[J].Philosophy Magazine,1933,16（105）:504-518.
[17]	OHNESORGE W.The formation of drops on nozzles and the dissolution of liquid rays[J].Journal of Applied Mathematics and Mechanics,1936,16（4）:355-358.
[18]	CHEHROUDI B,TALLEY D,COY E.Fractal geometry and growth rate changes of cryogenic jets near the critical point [R].Los Angeles,California,US:the 35th AIAA Joint Propulsion Conference and Exhibit,1999.
[19]	MAYER W,SCHIK A.Atomization and breakup of cryogenic propellants under high-pressure subcritical and supercritical conditions[J].Journal of Propulsion and Power,1998,14（5）:835-842.
[20]	VIGNESH M J,MORGAN R,VOGIATZAKI K,et al.Physics and modelling of cryogenic sprays[R].Brighton,UK:the 16th Spray SIG （Special Interest Group） Workshop,2019.
[21]	李佳楠,雷凡培,周立新,等.液体火箭发动机背压振荡环境下的雾化特性研究进展[J].推进技术,2019,40（11）:2401-2419.
[22]	康忠涛,李向东,毛雄兵.液体火箭发动机中气液同轴直流式喷嘴研究综述[J].航空学报,2018,39（9）:6-25.
[23]	杨立军,富庆飞.液体火箭发动机推力室设计[M].北京：北京航空航天大学出版社，2013.
[24]	CHOO Y J,KANG B S.A study on the velocity characteristics of the liquid elements produced by two impinging jets[J].Experiments in Fluids,2003,34（6）:655-661.
[25]	赵飞,刘昶秀,左光,等.液体火箭发动机互击式喷嘴喷雾特性研究[R].辽宁大连：中国航天第三专业信息网第38届技术交流会暨第2届空天动力联合会议,2017.
[26]	HEIDMANN M F,PRIEM R J，HUMPHREY J C.A study of sprays formed by two impinging jets[R].Washington D C：National Advisory Committee for Aeronautics,1957.
[27]	LI R,ASHGRIZ N.Characteristics of liquid sheets formed by two impinging jets[J].Physics of Fluids,2006,18（8）:1-14.
[28]	DOMBROWSKI N,JOHNS W R.The aerodynamic instability and disintegration of viscous liquid sheets[J].Chemical Engineering Science,1963,18（3）:203-214.
[29]	石少平.低Weber数射流撞击雾化的数学模型[J].航空动力学报,1994,9（3）:285-289.
[30]	BOUST B,MICHALSKI Q,CLAVERIE A,et al.Characterization of liquid impinging jet injector sprays for bi-propellant space propulsion:comparison of PDI and high-magnification shadowgraphy[R].Valencia,Spain:ILASS（Liquid Atomization and Spray Systems）-European Conference on Liquid Atomization and Spray Systems,2017.
[31]	LIU Xiufang,XUE Rong,RUAN Yixiao,et al.Effects of injection pressure difference on droplet size distribution and spray cone angle in spray cooling of liquid nitrogen[J].Cryogenics,2017,83:57-63.
[32]	GHODBANE M,HOLMAN J P.Experimental study of spray cooling with Freon-113[J].International Journal of Heat and Mass Transfer,1991,34（4/5）:1163-1174.
[33]	QIAO Y M,CHANDRA S.Spray cooling enhancement by addition of a surfactant[J].Journal of Heat Transfer,1998,120（1）:92-98.
[34]	REES A,ARANEO L,KURUDZIJA E,et al.Investigation of velocity and droplet size distributions of flash boiling LN2-jets with phase doppler anemometry[R].Paris,France:ILASS（Liquid Atomization and Spray Systems）-Europe 29th Conference on Liquid Atomization and Sprays Systems,2019.
[35]	CHEN R H,CHOW L C,NAVEDO J E.Effects of spray characteristics on critical heat flux in subcooled water spray cooling[J].International Journal of Heat and Mass Transfer,2002,45（19）:4033-4043.
[36]	ROSA M D,SENDER J,ZIMMERMANN H,et al.,Cryogenic spray ignition at high altitude conditions[R].Sacramento,California,US:the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit,2006.
[37]	ROY A,SEGAL C,JOLY C.Spreading angle and core length analysis of supercritical jets[J].AIAA Journal,2013,51（8）:2009-2014.
[38]	CHEHROUDI B,TALLEY D,COY E.Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures[J].Physics of Fluids,2002,14（2）:850-861.
[39]	SALLAM K A,DAI Z,FEATH G M.Liquid breakup at the surface of turbulent round liquid jets in still gases[J].International Journal of Multiphase Flow,2002,28（3）:427-449.
[40]	JAVAPRAKASH N,CHAKRAVARTHY S.Impingement atomization of gel fuels[R].Reno:Aerospace Science Meeting and Exhibit,2013.
[41]	YOON Y,JEUNG I.Effects of ambient gas pressure on the breakup of sprays in like-doublet and swirl coaxial injectors[R].Istanbul,Turkey:International Symposium on Energy Conversion Fundamentals,2004.
[42]	刘娟，李清廉，刘卫东,等.离心式喷嘴液膜破碎过程实验[J].推进技术,2011,32（4）:539-543.
[43]	YANG Shangze,LI Xuesong,HUNG L S D,et al.Characteristics and correlation of nozzle internal flow and jet breakup under flash boiling conditions[J].International Journal of Heat and Mass Transfer,2018,127:959-969.
[44]	AGARWAL A,TRUJILLO M F.A closer look at linear stability theory in modeling spray atomization[J].International Journal of Multiphase Flow,2018,109:1-13.
[45]	伏雨,于安,季斌,等.基于Level set方法的不同湍流模型在水翼空化流计算中的应用研究[J].水动力学研究与进展:A辑,2019,34（4）:430-439.
[46]	SHAO Changxiao,LUO Kun,YANG Jianshan,et al.Accurate level set method for simulations of liquid atomization[J].Chinese Journal of Chemical Engineering,2015,23（4）:597-604.
[47]	MIRJALILI S,JAIN S S,DODD M S.Interface-capturing methods for two-phase flows:an overview and recent developments[R].Palo Alto,US:Stanford University CTR （Center for Turbulence Research）,2017.
[48]	G?RTNER J W,REES A,KRONENBURG A,et al.Large eddy simulation of flashing cryogenic liquid with a compressible volume of fluid solver[R].Paris，France:the 29th Conference on Liquid Atomization and Spray Systems,2019.
[49]	CHU Wei,LI Xiuqian,TONG Yiheng,et al.Numerical investigation of the effects of gas-liquid ratio on the spray characteristics of liquid-centered swirl coaxial injectors.[J] Acta Astronautica,2020,175（9）:204-215.
[50]	王婕.对撞式喷嘴雾化特性的实验研究与数值模拟[D].南京：南京理工大学，2017.
[51]	LING Y,ZALESKI S,SCARDOVELLI R.Multiscale simulation of atomization with small droplets represented by a Lagrangian point-particle model[J].International Journal of Multiphase Flow,2015,76:122-143.
[52]	魏明锐,沃傲波,文华.燃油喷雾初始破碎及二次雾化机理的研究[J].内燃机学报,2009,27（2）:128-133.
[53]	SHINJO J,UMEMURA A.Simulation of liquid jet primary breakup:dynamics of ligament and droplet formation[J].International Journal of Multiphase Flow,2010,36（7）:513-532.
[54]	POPINET S.Gerris:a tree-based adaptive solver for the incompressible Euler equations in complex geometries[J].Journal of Computational Physics,2003,190（2）:572-600.
[55]	王凯,杨国华，李鹏飞，等.基于Gerris的离心式喷嘴锥形液膜破碎过程数值模拟[J].推进技术,2018,39（5）:1041-1050.
[56]	阮灿.液体射流撞击破碎雾化过程数值模拟[D].福建厦门：厦门大学，2017.
[57]	CHEN Xiaodong,MA Dongjun,YANG V.Mechanism study of impact wave in impinging jets atomization[R].Nashville,Tennessee,US:the 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,2012.
[58]	文键，王斯民，厉彦忠.基于MUSIG模型的低温流体过冷沸腾数值模拟[J].化学工程,2010,38 （11）:29-33.
[59]	马相孚.低温流体空化特性数值研究[D].哈尔滨：哈尔滨工业大学,2013.
[60]	余柳.LN_2-VN_2液泛过程的数值模拟及实验研究[D].杭州：浙江大学,2019.
[61]	GRAZIA L.Cryogenic flashing jets:a review[R].Salt Lake City,US:the 52nd AIAA/SAE/ASEE Joint Propulsion Conference,2016.
[62]	MAYER W,TELAR J,BRANAM R,et al.Raman measurements of cryogenic injection at supercritical pressure[J].Heat and Mass Transfer,2003,39（8）:709-719.
[63]	FDIDA N,MAURIOT Y,VINGERT L,et al.Characterizing primary atomization of cryogenic LOX/Nitrogen and LOX/helium sprays by visualizations coupled to Phase Doppler Interferometry[J].Acta Astronautica,2018,164:458-465.
[64]	SCHMIDT V,KLIMENKO D N,HAIDN O,et al.Experimental investigation and modelling of the ignition transient of a coaxial H₂/O₂-injector[R].Chattanooga,US：5th International Symposium on Liquid Rocket Propulsion,2003.
[65]	SCHMIDT V,WEPLER U,HAIDN O J,et al.Characterization of the primary ignition process of a coaxial GH₂/LOX spray[R].Reno,US:the 42nd AIAA/ASME/SAE/ASEE Aero Space Sciences Meeting,2004.
[66]	RONG X,YI X R,LIU X F,et al.Experimental study of liquid nitrogen spray characteristics in atmospheric environment[J].Applied Thermal Engineering,2018,142:717-722.
[67]	JIN T,ZHANG S Y,TANG K,et al.Observation and analysis of the detachment frequency of coalesced bubbles in pool boiling liquid nitrogen[J].Cryogenics,2011,51:516-520.
[68]	REES A,SALZMANN H,SENDER J,et al.Investigation of flashing LN₂-jets in terms of spray morphology,droplet size and velocity distributions[R].Madrid,Spain：the 8th European Conference for Aeronautics and Space Sciences（EUCASS）,2019.