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

横向流场中矩形喷嘴液体射流破碎特征的数值研究

邵猛 何志霞 王谦

邵猛, 何志霞, 王谦. 横向流场中矩形喷嘴液体射流破碎特征的数值研究[J]. 航空动力学报, 2025, 40(12):20240073 doi: 10.13224/j.cnki.jasp.20240073
引用本文: 邵猛, 何志霞, 王谦. 横向流场中矩形喷嘴液体射流破碎特征的数值研究[J]. 航空动力学报, 2025, 40(12):20240073 doi: 10.13224/j.cnki.jasp.20240073
SHAO Meng, HE Zhixia, WANG Qian. Numerical study on liquid jet breakup characteristics of rectangular nozzles in crossflow[J]. Journal of Aerospace Power, 2025, 40(12):20240073 doi: 10.13224/j.cnki.jasp.20240073
Citation: SHAO Meng, HE Zhixia, WANG Qian. Numerical study on liquid jet breakup characteristics of rectangular nozzles in crossflow[J]. Journal of Aerospace Power, 2025, 40(12):20240073 doi: 10.13224/j.cnki.jasp.20240073

横向流场中矩形喷嘴液体射流破碎特征的数值研究

doi: 10.13224/j.cnki.jasp.20240073
基金项目: 国家自然科学基金(51876083)
详细信息
    作者简介:

    邵猛(1994-),男,博士生,主要从事横向流场中液体射流破碎机制的研究。E-mail:sm615243@126.com

    通讯作者:

    王谦(1968-),男,教授,博士,研究领域为动力机械燃油喷射与燃烧理论及技术。E-mail:qwang@ujs.edu.cn

  • 中图分类号: V434.1

Numerical study on liquid jet breakup characteristics of rectangular nozzles in crossflow

  • 摘要:

    通过数值模拟研究了矩形喷嘴在横向流场中的液体射流。着重分析了喷嘴的纵横比对液柱初次破碎过程中破碎行为及变形特征的影响。纵横比的范围为1~8。结果表明:在较低风速下,表面破碎几乎不受矩形喷嘴纵横比的影响,柱破碎模式由袋状破碎逐渐向着“两条纹一膜”(two-streak-one-membrane)结构转变。在较高风速下,表面破碎较为强烈。随着纵横比增加,表面破碎先减弱后增强,柱破碎模式由“两条纹一膜”(two-streak-one-membrane)结构向着“三条纹两膜”(three-streak-two-membrane)结构转变。随着射流的延伸,液柱宽度逐渐增加。矩形喷嘴的纵横比越大,表面张力越大,横流对液柱变形的促进作用越弱,液柱宽度增加的趋势也就越缓。液柱厚度的变化不仅与喷嘴纵横比有关,还受到射流过程中柱破碎模式的影响。此外,随着风速的增加,矩形喷嘴的纵横比对表面破碎和柱破碎起始点的影响逐渐减弱。

     

  • 图 1  计算域示意图

    Figure 1.  Schematic diagram of computational domain

    图 2  计算网格示意图

    Figure 2.  Schematic diagram of the computational mesh

    图 3  三级自适应加密网格示意图

    Figure 3.  Schematic of mesh with AMR method of level 3

    图 4  不同网格参数下迎风轨迹的比较

    Figure 4.  Comparison of the windward trajectory with different mesh parameters

    图 5  不同网格参数下的截面形状

    Figure 5.  Shape of cross section for different mesh parameters

    图 6  数值计算的迎风轨迹与Eslamian等[17]实验数据

    Figure 6.  Windward trajectory of numerical results and the experimental data by Eslamian et al. [17]

    图 7  液体射流的侧视图

    Figure 7.  Side view of liquid jet

    图 8  横流中液体射流侧视图

    Figure 8.  Side view of liquid jet in crossflow

    图 9  局部放大图

    Figure 9.  Zoomed-in views

    图 10  横流中液体射流的左视图

    Figure 10.  Left view of liquid jet in crossflow

    图 11  表面破碎和柱状破碎起始点示意图

    Figure 11.  Schematic of onset of surface breakup and column breakup

    图 12  表面破碎起始点的变化

    Figure 12.  Variation of onset of surface breakup point

    图 13  柱破碎起始点的变化

    Figure 13.  Variation of onset of column breakup point

    图 14  不同射流高度下液柱截面形状

    Figure 14.  Cross section shape of liquid column at different penetration height

    图 15  液柱宽度的变化

    Figure 15.  Variation of liquid column width

    图 16  液柱厚度的变化

    Figure 16.  Variation of liquid column thickness

    表  1  喷嘴的几何参数

    Table  1.   Geometrical parameters of nozzles

    L/mm W/mm R Dh/mm An/mm2
    0.300 0.300 1 0.300 0.09
    0.212 0.424 2 0.283
    0.150 0.600 4 0.240
    0.122 0.735 6 0.210
    0.106 0.849 8 0.189
    下载: 导出CSV

    表  2  物性参数及边界条件

    Table  2.   Physical parameters and boundary conditions

    参数 数值
    ρl/(kg/m3 998
    ρg/(kg/m3 1.2
    ul/(m/s) 10
    ug/(m/s) 40, 60, 80
    σl/(N/m) 0.072
    pout/Pa 0
    下载: 导出CSV

    表  3  网格参数

    Table  3.   Mesh parameters

    网格序列
    编号
    初始网格
    尺寸/mm
    自适应
    加密等级
    加密后网格
    尺寸/μm
    M1 0.10 1 50.00
    M2 0.10 2 25.00
    M3 0.10 3 12.50
    M4 0.08 3 10.00
    下载: 导出CSV
  • [1] 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. WANG Xionghui, HUANG Yong, WANG Fang, et al. Bag breakup of round liquid jets in crossflow[J]. Journal of Propulsion Technology, 2012, 33(2): 198-204. (in Chinese

    WANG Xionghui, HUANG Yong, WANG Fang, et al. Bag breakup of round liquid jets in crossflow[J]. Journal of Propulsion Technology, 2012, 33(2): 198-204. (in Chinese)
    [2] HU Bihe, HE Zhixia, LI Chen, et al. Study of the effect of cavitation flow patterns in diesel injector nozzles on near-field spray atomization characteristics using a LES-VOF method[J]. International Journal of Multiphase Flow, 2024, 174: 104791. doi: 10.1016/j.ijmultiphaseflow.2024.104791
    [3] SONG J, CARY CAIN C, GUEN LEE J. Liquid jets in subsonic air crossflow at elevated pressure[J]. Journal of Engineering for Gas Turbines and Power, 2015, 137(4): 041502. doi: 10.1115/1.4028565
    [4] ALMEIDA H, SOUSA J M M, COSTA M. Effect of the liquid injection angle on the atomization of liquid jets in subsonic crossflows[J]. Atomization and Sprays, 2014, 24(1): 81-96. doi: 10.1615/AtomizSpr.2013008310
    [5] WIEST H K, HEISTER S D. Experimental study of a heated liquid jet in a crossflow: AIAA 2015-3864 [R]. Orlando, US: 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015.
    [6] LI Xiaoyi, SOTERIOU M C. Detailed numerical simulation of liquid jet atomization in crossflow of increasing density[J]. International Journal of Multiphase Flow, 2018, 104: 214-232. doi: 10.1016/j.ijmultiphaseflow.2018.02.016
    [7] YU Shenghao, YIN Bifeng, DENG Weixin, et al. Experimental study on the spray and mixing characteristics for equilateral triangular and circular nozzles with diesel and biodiesel under high injection pressures[J]. Fuel, 2019, 239: 97-107. doi: 10.1016/j.fuel.2018.10.146
    [8] YU Shenghao, YIN Bifeng, DENG Weixin, et al. Experimental study on the diesel and biodiesel spray characteristics emerging from equilateral triangular orifice under real diesel engine operation conditions[J]. Fuel, 2018, 224: 357-365. doi: 10.1016/j.fuel.2018.03.099
    [9] NEW T H, LIM T T, LUO S C. Elliptic jets in cross-flow[J]. Journal of Fluid Mechanics, 2003, 494: 119-140. doi: 10.1017/S0022112003005925
    [10] MORAD M R, KHOSROBEYGI H. Penetration of elliptical liquid jets in low-speed crossflow[J]. Journal of Fluids Engineering, 2019, 141: 011301. doi: 10.1115/1.4040373
    [11] OLYAEI G, KEBRIAEE A. Experimental study of liquid jets injected in crossflow[J]. Experimental Thermal and Fluid Science, 2020, 115: 110049. doi: 10.1016/j.expthermflusci.2020.110049
    [12] 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.
    [13] BRACKBILL J U, KOTHE D B, ZEMACH C. A continuum method for modeling surface tension[J]. Journal of Computational Physics, 1992, 100(2): 335-354. doi: 10.1016/0021-9991(92)90240-Y
    [14] SYAWITRI T P, YAO Yufeng, YAO Jun, et al. Assessment of stress-blended eddy simulation model for accurate performance prediction of vertical axis wind turbine[J]. International Journal of Numerical Methods for Heat & Fluid Flow, 2021, 31(2): 655-673.
    [15] GOSMAN A D, LOANNIDES E. Aspects of computer simulation of liquid-fuelled combustors[J]. AIAA Journal, 1981, 81: 482-490.
    [16] SALLAM K, NG C, SANKARAKRISHNAN R, et al. Breakup of turbulent and non-turbulent liquid jets in gaseous crossflows: AIAA 2006-1517 [R]. Reno, US: 44th AIAA Aerospace Sciences Meeting and Exhibit, 2006.
    [17] ESLAMIAN M, AMIGHI A, ASHGRIZ N. Atomization of liquid jet in high-pressure and high-temperature subsonic crossflow[J]. AIAA Journal, 2014, 52(7): 1374-1385. doi: 10.2514/1.J052548
    [18] XIAO F, DIANAT M, MCGUIRK J J. Large eddy simulation of liquid-jet primary breakup in air crossflow[J]. AIAA Journal, 2013, 51(12): 2878-2893. doi: 10.2514/1.J052509
    [19] BEHZAD M, ASHGRIZ N, KARNEY B W. Surface breakup of a non-turbulent liquid jet injected into a high pressure gaseous crossflow[J]. International Journal of Multiphase Flow, 2016, 80: 100-117. doi: 10.1016/j.ijmultiphaseflow.2015.11.007
  • 加载中
图(16) / 表(3)
计量
  • 文章访问数:  466
  • HTML浏览量:  226
  • PDF量:  24
  • 被引次数: 0
出版历程
  • 收稿日期:  2024-02-02
  • 网络出版日期:  2025-09-29

目录

    /

    返回文章
    返回