留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

偏心撞击对撞击式喷嘴雾化特性的影响

李佳楠 雷凡培

李佳楠, 雷凡培. 偏心撞击对撞击式喷嘴雾化特性的影响[J]. 航空动力学报, 2019, 34(10): 2280-2293. doi: 10.13224/j.cnki.jasp.2019.10.022
引用本文: 李佳楠, 雷凡培. 偏心撞击对撞击式喷嘴雾化特性的影响[J]. 航空动力学报, 2019, 34(10): 2280-2293. doi: 10.13224/j.cnki.jasp.2019.10.022
LI Jianan, LEI Fanpei. Effects of misaligned impingement on atomization characteristics of impinging jet injector[J]. Journal of Aerospace Power, 2019, 34(10): 2280-2293. doi: 10.13224/j.cnki.jasp.2019.10.022
Citation: LI Jianan, LEI Fanpei. Effects of misaligned impingement on atomization characteristics of impinging jet injector[J]. Journal of Aerospace Power, 2019, 34(10): 2280-2293. doi: 10.13224/j.cnki.jasp.2019.10.022

偏心撞击对撞击式喷嘴雾化特性的影响

doi: 10.13224/j.cnki.jasp.2019.10.022
基金项目: 国家重大基础研究项目(613193)

Effects of misaligned impingement on atomization characteristics of impinging jet injector

  • 摘要: 为研究偏心撞击对撞击式喷嘴雾化特性的影响,建立了求解自燃推进剂冷态射流撞击雾化过程的数值模拟方案,计算了不同偏心度条件下的射流撞击雾化过程。采用树形自适应加密算法直接求解不可压Navier-Stokes方程组,由分段线性的流体体积(VOF)方法对流体界面进行捕捉。结果表明偏心撞击会导致雾场发生偏转,当无量纲偏心度E为1/8时,雾场偏转角度约为9.2°,应控制加工偏差小于该值。随着偏心度的增大,液膜的偏转角度增大,理论推导得到的液膜偏转角度要小于数值计算得到的液膜偏转角度。正心撞击时燃料与氧化剂流强峰值接近,雾场的流强分布呈单峰分布。当发生偏心撞击时,由于燃料与氧化剂部分射流未参与撞击导致流强峰值出现交错,雾场的流强分布呈双峰分布,混合比的空间分布发生较大改变。正心撞击时撞击点下游液滴的速度分布近似呈轴对称分布,而偏心撞击之后的速度分布则呈中心对称分布。偏心撞击导致的射流动量损失使得雾化性能变差,当无量纲偏心度E为1/8时,一甲基肼(MMH)的Sauter平均直径增大约4.8%,四氧化二氮(NTO)的Sauter平均直径增大约5.8%。

     

  • [1] HEIDMANN M F,PRIEM R J,HUMPHREY J C.A study of sprays formed by two impinging jets[R].NACA (National Advisory Committee for Aeronautics) TN3835,1957.
    [2] HEIDMANN M F,HUMPHREY J C.Fluctuations in a spray formed by two impinging jets[R].NACA (National Advisory Committee for Aeronautics) TN2349,1951.
    [3] ANDERSON W E,RYAN H M,SANTORO R J.Impact wave-based model of impinging jet atomization[J].Atomization and Sprays,2006,16(7):791-805.
    [4] RYAN H M,ANDERSON W E,PAL S,et al.Atomization characteristics of impinging liquid jets[J].Journal of Propulsion and Power,1995,11(1):135-145.
    [5] LI R,ASHGRIZ N.Characteristics of liquid sheets formed by two impinging jets[J].Physics of Fluids,2006,18(8):087104.1-087104.13
    [6] PANO M R O,DELGADO J M D.Effect of pre-impingement length and misalignment in the hydrodynamics of multijet impingement atomization[J].Physics of Fluids,2013,25(1):012105.1-012105.11
    [7] SUBEDI B,SON M,KIM W,et al.Spray characteristics of misaligned impinging injectors[J].Journal of the Korean Society of Marine Engineering,2014,38(10):1257-1262.
    [8] 邓寒玉,封锋,武晓松,等.射流偏心撞击对凝胶推进剂撞击雾化影响的实验研究[J].兵工学报,2016,37(4):612-620.DENG Hanyu,FENG Feng,WU Xiaosong,et al.Experimental research on the effect of eccentric impact of jet on the impinging atomization of gel propellant[J].Acta Armamentarii,2016,37(4):612-620.(in Chinese)
    [9] INOUE C,WATANABE T,HIMENO T.Study on atomization process of liquid sheet formed by impinging jets[R].AIAA 2008-4847,2008.
    [10] ARIENTI M,LI X,SOTERIOU M C,et al.Coupled level-set/volume-of-fluid method for the simulation of liquid atomization in propulsion device injectors[R].AIAA 2010-7136,2010.
    [11] CHEN X D,MA D J,YANG V.Mechanism study of impact wave in impinging jets atomization[R].AIAA 2012-1089,2012.
    [12] CHEN X D,MA D J,YANG V.High-fidelity numerical simulations of impinging jet atomization[R].AIAA 2012-4328,2012.
    [13] CHEN X D,YANG V.Thickness-based adaptive mesh refinement methods for multi-phase flow simulations with thin regions[J].Journal of Computational Physics,2014,269:22-39.
    [14] 郑刚,聂万胜,何博,等.撞击角对撞击式喷嘴雾化特性影响研究[J].推进技术,2015,36(4):608-613.ZHENG Gang,NIE Wansheng,HE Bo,et al.Effects of impingement angle on atomization characteristics of impinging jets injector[J].Journal of Propulsion Technology,2015,26(4):608-613.(in Chinese)
    [15] 郑刚,冯伟,聂万胜,等.动量比对两股互击式喷嘴雾化特征的影响[J].航空动力学报,2016,31(9):2283-2289.ZHENG Gang,FENG Wei,NIE Wansheng,et al.Effect of momentum ratio on atomization characteristics of unlike-doublet impinging jets injector[J].Journal of Aerospace Power,2016,31(9):2283-2289.(in Chinese)
    [16] ZHENG G,NIE W S,FENG S J,et al.Numerical simulation of the atomization process of a like-doublet impinging rocket injector[J].Procedia Engineering,2015,99:930-938.
    [17] 刘昌波,雷凡培,周立新.两股湍流射流撞击雾化过程的数值研究[J].推进技术,2014,35(12):1669-1678.LIU Changbo,LEI Fanpei,ZHOU Lixin,et al.Primary atomization simulations of two turbulent impinging jets[J].Journal of Propulsion Technology,2014,35(12):1669-1678.(in Chinese)
    [18] 强洪夫,刘虎,陈福振,等.基于SPH方法的射流撞击仿真[J].推进技术,2012,33(3):424-429.QIANG Hongfu,LIU Hu,CHEN Fuzhen,et al.Simulation on jet impingement based on SPH method[J].Journal of Propulsion Technology,2012,33(3):424-429.(in Chinese)
    [19] 强洪夫,韩亚伟,王广,等.幂律型流体雾化SPH方法数值分析[J].推进技术,2013,34(2):240-247.QIANG Hongfu,HAN Yawei,WANG Guang,et al.Numerical simulationof atomization process of liquid with power law model based on SPH method[J].Journal of Propulsion Technology,2013,34(2):240-247.(in Chinese)
    [20] 韩亚伟,强洪夫,刘虎.双股液体射流撞击雾化的SPH方法数值模拟[J].工程力学,2013,30(3):17-23.HAN Yawei,QIANG Hongfu,LIU Hu.Numerical simulation of two liquid impinging jets with SPHmethod[J].Engineering Mechanics,2013,30(3):17-23.(in Chinese)
    [21] WEI Q,LIANG G Z.Coupled lagrangian impingement spray model for doublet impinging injectors under liquid rocket engine operating conditions[J].Chinese Journal of Aeronautics,2017,30(4):1391-1406.
    [22] YUAN T,CHEN C,HUANG B.Optical observation of the impingements of nitrogentetroxide/monomethylhyd-razine simulants[J].AIAA Journal,2006,44(10):2259-2266.
    [23] YUAN T,CHEN C,HUANG B.Comparison of hot-fire and cold-flow observations of nitrogentetroxide/ monomethylhydrazine impinging combustion[J].AIAA Journal,2009,47(10):2359-2367.
    [24] YUAN T,CHEN C,HUANG B,et al.The impinging-type injector design of MMH/NTO liquid rocket engine[R].AIAA 2012-3745,2012.
    [25] RUPE J H.An experimental correlation of the nonreactive properties of injection schemes and combustion effects in a liquid-propellant rocket engine:Part 1 the application of nonreactive-spray properties to rocket-motor injector design[R].NASA-CR-64635,1965.
    [26] TANI H,DAIMON Y,SASAKI M,et al.Atomization and hypergolic reactions of impinging streams of monomethylhydrazine and dinitrogen tetroxide[J].Combustion and Flame,2017,185:142-151.
    [27] 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.
    [28] POPINET S.An accurate adaptive solver for surface-tension-driven interfacial flows[J].Journal of Computational Physics,2009,228(16):5838-5866.
    [29] BRACKBILL J U,KOTHE D B,ZEMACH C A.A continuum method for modeling surface tension[J].Journal of Computational Physics,1992,100(2):335-354.
    [30] 阎超,于剑,徐晶磊,等.CFD模拟方法的发展成就与展望[J].力学进展,2011,41(5):563-589.YAN Chao,YU Jian,XU Jinglei,et al.On the achievements and prospects for the methods of computational fluid dynamics[J].Advances in Mechanics,2011,41(5):563-589.(in Chinese)
    [31] BORIS J P,GRINSTEIN F F,ORAN E S,et al.New insights into large eddy simulation[R].NAL(Naval Research Laboratory),4400-92-6979,1992
    [32] HIRT C W,NICHOLS B D.Volume of fluid (VOF) method for the dynamics of free boundaries[J].Journal of Computational Physics,1981,39(1):201-225.
    [33] ANDERSON W E.Theeffectsof atomization on combustion stability[D].Philadelphia:The Pennsylvania State University,1996:30-34.
    [34] ANDERSON W E,RYAN H M,SANTORO R J,et al.Combustion instability mechanisms in liquid rocket engines using impinging jet injectors[R].AIAA 95-2357,1995.
    [35] ZHANG P Y,WANG B.Effects of elevated ambient pressure on the disintegration of impinged sheets[J].Physics of Fluids,2017,29:042202.1-042202.17.
    [36] RUPE J H.The liquid-phase mixing of impinging streams[R].Pasadena,US:Jet Propulsion Laboratory,Progress Report,1953.
    [37] RUPE J H.A correlation between the dynamic properties of a pair of impinging streams and the uniformity of mixture-ratio distribution in resulting spray[R].Pasadena,US:Jet Propulsion Laboratory,Progress Report,1956.
    [38] 费俊,孙璠,杨伟东,等.射流撞击雾化液滴运动过程与粒径分布特性的试验研究[J].火箭推进,2015,41(1):10-14,35.FEI Jun,SUN Fan,YANG Weidong,et al.Experimental analysis on movement and size distribution of atomized droplets from impinging liquid jet[J].Journal of Rocket Propulsion,2015,41(1):10-14,35.(in Chinese)
  • 加载中
计量
  • 文章访问数:  441
  • HTML浏览量:  4
  • PDF量:  332
  • 被引次数: 0
出版历程
  • 收稿日期:  2019-02-19
  • 刊出日期:  2019-10-28

目录

    /

    返回文章
    返回