Volume 31 Issue 9
Sep.  2016
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2016  >  31(9): 2283-2289
ZHENG Gang, FENG Wei, NIE Wan-sheng, ZHOU Li-xin. Effect of momentum ratio on atomization characteristics of unlike-doublet impinging jets injector[J]. Journal of Aerospace Power, 2016, 31(9): 2283-2289. doi: 10.13224/j.cnki.jasp.2016.09.030
Citation: ZHENG Gang, FENG Wei, NIE Wan-sheng, ZHOU Li-xin. Effect of momentum ratio on atomization characteristics of unlike-doublet impinging jets injector[J]. Journal of Aerospace Power, 2016, 31(9): 2283-2289. doi: 10.13224/j.cnki.jasp.2016.09.030
shu

Effect of momentum ratio on atomization characteristics of unlike-doublet impinging jets injector

doi: 10.13224/j.cnki.jasp.2016.09.030

  • 1. Department of Space Equipment, Equipment Academy, Beijing 101416, China;

  • 2. Technology Department, Xichang Satellite Launch Center, Xichang Sichuan 615000, China;

  • 3. Xi'an Aerospace Propulsion Institute, China Aerospace Science and Technology Corporation, Xi'an 710100, China

  • Received Date: 2015-04-26
  • Publish Date: 2016-09-28
    Abstract
  • Numerical simulation was carried out on the atomization process of unlike-doublet impinging jets injector based on the CLSVOF (coupled level-set and volume of fluid) method. The simulation results were compared with the experiment results, and the effect of momentum ratios on liquid sheet characteristics was investigated in detail. The results show that:(1) The CLSVOF method can efficiently capture the liquid sheet characteristics formed by jet impact. The calculated liquid sheet agrees well with the experiment result. (2) In the impinging process of jets, part of the jet flow of large diameter nozzle is not involved in the impact, while the velocity of liquid in the central position drops rapidly after impact, and at the same time, the surrounding liquid maintains the velocity before impact, which results in the formation of cured liquid sheet. (3) Under the conditions of different momentum ratios, the resultant angle in the axis position after impact mainly depends on the momentum ratio of impinging jets. The simulation results are in good agreement with the theoretical calculation results, with the errors less than 10%.

     

    • FullText(HTML)
  • loading
    • References(18)
  • [1]
    杨V,安德松W E.液体火箭发动机燃烧不稳定性[M].张宝炯,洪鑫,陈杰,译.北京:科学出版社,2001.
    [2]
    石少平,庄逢辰.射流撞击雾化索太尔平均直径的计算[J].推进技术,1995,16(3):22-25. SHI Shaoping,ZHUANG Fengchen.Calculation of the Sauter mean diameter of jet-impinging atomizers[J].Journal of Propulsion Technology,1995,16(3):22-25.(in Chinese)
    [3]
    Donald J H.Spray characterization of like-on-like doublet impinging rocket injector[R].AIAA 91-0687,1991.
    [4]
    Lai W H,Wang H C.Flow patterns generated by like and unlike-doublet impinging jets[R].AIAA-2002-3700,2002.
    [5]
    Li R,Nasser A.Characteristics of liquid sheet formed by two impinging jets[J].Physics of Fluid,2006,18(8):1-13.
    [6]
    张蒙正,张泽平.两股互击式喷嘴雾化性能实验研究[J].推进技术,2000,21(1):57-59. ZHANG Mengzheng,ZHANG Zeping.Experimental research on spray properties of unlike impinging injectors[J].Journal of Propulsion Technology,2000,21(1):57-59.(in Chinese)
    [7]
    张蒙正,杨伟东,王玫.双股互击式喷嘴凝胶水雾化特性实验[J].推进技术,2008,29(1):22-24. ZHANG Mengzheng,YANG Weidong,WANG Mei.Test of unlike impinging injector atomization characteristics with gelled water[J].Journal of Propulsion Technology,2008,29(1):22-24.(in Chinese)
    [8]
    刘晓伟,胡伟,曹晶,等.鲁泊数和孔径比对直流互击式喷注器性能的影响[J].火箭推进,2010,36(3):24-27. LIU Xiaowei,HU Wei,CAO Jing,et al.Effects of Rupe number and ratio of injection orifice diameter on unlike impinging injector performance[J].Journal of Rocket Propulsion,2010,36(3):24-27.(in Chinese)
    [9]
    Lebas R,Menard T,Beau P A,et al.Numerical simulation of primary break-up and atomization:DNS and modeling study[J].International Journal of Multiphase Flow,2009,35(3):247-260.
    [10]
    LI Qiang,OUYANG Jie,YANG Binxin,et al.Numerical simulation of gas-assisted injection molding using CLSVOF method[J].Applied Mathematical Modelling,2012,36(5):2264-2274.
    [11]
    CHEN Xiaodong,MA Dongjun,Yang V.Mechanism study of impact wave in impinging jets atomization[R].AIAA-2012-1089,2012.
    [12]
    Chihiro I,Toshinori W,Takehiro H.Liquid sheet dynamics and primary breakup characteristics at impingement type injector[R].AIAA-2009-5014,2009.
    [13]
    Chihiro I,Toshinori W,Takehiro H.Study on atomization process of liquid sheet formed by impinging jets[R].AIAA-2008-4847,2008.
    [14]
    魏锦洲,王占学.两股互击式喷嘴雾化数值模拟研究[J].机械设计与制造,2009(8):130-132. WEI Jinzhou,WANG Zhanxue.Numerical simulation for spray characteristic of like-doublet injector[J].Machinery Design and Manufacture,2009(8):130-132.(in Chinese)
    [15]
    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)
    [16]
    Sussman M,Puckett E.A coupled level set and volume-of-fluid method for computing 3D and axisymmetric incompressible two-phase flow[J].Journal of Computational Physics,2000,162(2):301-337.
    [17]
    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.
    [18]
    张蒙正,傅永贵,张泽平,等.两股互击式喷嘴雾化研究及应用[J].推进技术,1999,20(2):73-75. ZHANG Mengzheng,FU Yonggui,ZHANG Zeping,et al.Spray property research and application of unlike impinging injector[J].Journal of Propulsion Technology,1999,20(2):73-75.(in Chinese)
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(1231.0KB)
    XML

    Article Metrics

    Article views (1108) PDF downloads(500) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return