Turn off MathJax
Article Contents
Zhang Xiao, Zhu Wei, Hu Haifeng, et al. Simulation and experiment on the atomization performance of liquid-liquid coaxial centrifugal dual injectors[J]. Journal of Aerospace Power, 2026, 41(X):20260072 doi: 10.13224/j.cnki.jasp.20260072
Citation: Zhang Xiao, Zhu Wei, Hu Haifeng, et al. Simulation and experiment on the atomization performance of liquid-liquid coaxial centrifugal dual injectors[J]. Journal of Aerospace Power, 2026, 41(X):20260072 doi: 10.13224/j.cnki.jasp.20260072

Simulation and experiment on the atomization performance of liquid-liquid coaxial centrifugal dual injectors

doi: 10.13224/j.cnki.jasp.20260072
  • Received Date: 2026-04-29
    Available Online: 2026-05-25
  • To investigate the atomization field of liquid-liquid coaxial centrifugal dual injectors, a cross-scale computational framework based on the VOF-to-DPM (volume of fluid to discrete phase model) method was constructed and validated through comparative analysis with cold-flow experiments. The simulation model achieved a spray cone angle error of within 0.85% and the Sauter mean diameter error of no more than 20%. The study found that for the liquid-liquid coaxial centrifugal injector, an increase in the flow rates of both the inner and outer injectors led to a gradual increase in the spray cone angle, while the droplet size simultaneously decreased in both the interaction and non-interaction zones. The influence of inter-injector distance on the atomization characteristics was also examined. Simulation results for different injectors spacings indicated that as the distance between the spray plumes increased, the spray cone angle gradually increased. The variation pattern of the Sauter mean diameter of the droplets was related to the state of liquid film interaction: when the interaction point lied within a continuous and stable liquid film, a larger injector spacing resulted in a smaller Sauter mean diameter; conversely, when the interaction occurred within an unstable, breaking liquid film, the trend was reversed.

     

  • loading
  • [1]
    朱宁昌. 液体火箭发动机设计: 上[M]. 北京: 中国宇航出版社, 1994.
    [2]
    庄逢辰. 液体火箭发动机喷雾燃烧的理论、模型及应用[M]. 长沙: 国防科技大学出版社, 1995.
    [3]
    Seo S, Kim S K, Choi H S. Combustion dynamics and stability of a fuel-rich gas generator[J]. Journal of Propulsion and Power, 2010, 26(2) : 259-266.
    [4]
    Fu Qingfei, Qiao Wentong, Li Penghui, et al. Review on the dynamic characteristics of liquid rocket engine injector[J]. Advances in Astronautics, 2025, 8(2): 129-169. doi: 10.1007/s42423-025-00181-7
    [5]
    Casiano M J, Hulka J R, Yang V. Liquid-propellant rocket engine throttling: a comprehensive review[J]. Journal of Propulsion and Power, 2010, 26(5): 897-923. doi: 10.2514/1.49791
    [6]
    Sivakumar D, Raghunandan B N. Hysteretic interaction of conical liquid sheets from coaxial atomizers: influence on the spray characteristics[J]. Physics of Fluids, 1998, 10(6): 1384-1397. doi: 10.1063/1.869663
    [7]
    Sivakumar D, Raghunandan B N. Formation and separation of merged liquid sheets developed from the mixing of coaxial swirling liquid sheets[J]. Physics of Fluids, 2003, 15(11): 3443-3451. doi: 10.1063/1.1616032
    [8]
    Ramamurthi K, Tharakan T J. Experimental study of liquid sheets formed in coaxial swirl injectors[J]. Journal of Propulsion and Power, 1995, 11(6): 1103-1109. doi: 10.2514/3.23947
    [9]
    Rashid M S F M, Hamid A H A, Ghaffar Z A, et al. An experimental investigation on spray characteristics emanating from liquid-liquid coaxial swirl atomizer[C]//Proceedings of the 4th International Meeting of Advances in Thermofluids (IMAT 2011). Melaka, Malaysia: American Institute of Physics, 2012: 591-598.
    [10]
    徐顺, 康忠涛, 成鹏, 等. 喷注压降对液液同轴离心式喷嘴喷雾锥角的影响研究[J]. 推进技术, 2017, 38(7): 1556-1562. Xu Shun, Kang Zhongtao, Cheng Peng, et al. Effects of injection pressure on spray angle of liquid-liquid swirl coaxial injector[J]. Journal of Propulsion Technology, 2017, 38(7): 1556-1562. (in Chinese

    Xu Shun, Kang Zhongtao, Cheng Peng, et al. Effects of injection pressure on spray angle of liquid-liquid swirl coaxial injector[J]. Journal of Propulsion Technology, 2017, 38(7): 1556-1562. (in Chinese)
    [11]
    Kim D, Jeong W, Im J, et al. The characteristics of swirl coaxial injector under varying geometric and environmental conditions[R]. AIAA 2004-3521, 2004.
    [12]
    Eberhart C, Lineberry D, Moser M. Effects of variable chamber pressure on swirl coaxial injection: a cold flow study[R]. AIAA-2010-6665, 2010.
    [13]
    Alves A, Lacava P T, Martins C A. Effects of the number of tangential passages on spray characteristics of a bipropellant atomizer[J]. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2014, 36(3): 583-590. doi: 10.1007/s40430-013-0101-3
    [14]
    Ahn K, Han Y M, Seo S, et al. Effects of injector recess and chamber pressure on combustion characteristics of liquid–liquid swirl coaxial injectors[J]. Combustion Science and Technology, 2010, 183(3): 252-270. doi: 10.1080/00102202.2010.516289
    [15]
    Kim D, Han P, Im J H, et al. Effect of recess on the spray characteristics of liquid-liquid swirl coaxial injectors[J]. Journal of Propulsion and Power, 2007, 23(6): 1194-1203. doi: 10.2514/1.30450
    [16]
    Vasques B B, de Mendonc¸a M T, da Costa Dourado W M. Numerical and experimental study of swirl atomizers for liquid propellant rocket engines[C]//Advances in Aerospace Technology; Energy Water Nexus; Globalization of Engineering; Posters. Denver, US: ASMEDC, 2011: 951-957.
    [17]
    汪凤山, 毛晓芳, 虞育松, 等. 双组元离心式喷注器雾化性能的大涡模拟数值研究[J]. 空间控制技术与应用, 2012, 38(6): 13-17. Wang Fengshan, Mao Xiaofang, Yu Yusong, et al. Numerical LES study of spray performance in a bi-propellant coaxial centrifugal injector[J]. Aerospace Control and Application, 2012, 38(6): 13-17. (in Chinese

    Wang Fengshan, Mao Xiaofang, Yu Yusong, et al. Numerical LES study of spray performance in a bi-propellant coaxial centrifugal injector[J]. Aerospace Control and Application, 2012, 38(6): 13-17. (in Chinese)
    [18]
    丁佳伟. 液/液同轴旋转射流稳定性及液膜破碎机理研究[D]. 北京: 北京交通大学, 2017. Ding Jiawei. Study on stability and liquid sheet breakup mechanism of liquid/liquid coaxial swirling jets[D]. Beijing: Beijing Jiaotong University, 2017. (in Chinese

    Ding Jiawei. Study on stability and liquid sheet breakup mechanism of liquid/liquid coaxial swirling jets[D]. Beijing: Beijing Jiaotong University, 2017. (in Chinese)
    [19]
    丁佳伟, 李国岫, 虞育松. 结构参数对双组元推力器喷注器雾化性能影响规律的数值模拟研究[J]. 载人航天, 2015, 21(6): 635-641. Ding Jiawei, Li Guoxiu, Yu Yusong. Numerical simulation for the influence of injector structure parameters on spray characteristics in bipropellant thruster[J]. Manned Spaceflight, 2015, 21(6): 635-641. (in Chinese

    Ding Jiawei, Li Guoxiu, Yu Yusong. Numerical simulation for the influence of injector structure parameters on spray characteristics in bipropellant thruster[J]. Manned Spaceflight, 2015, 21(6): 635-641. (in Chinese)
    [20]
    王壮, 党枭睿, 胡海峰, 等. 缩进长度对液液同轴离心喷嘴雾化过程的影响[J]. 火箭推进, 2024, 50(3): 42-52. Wang Zhuang, Dang Xiaorui, Hu Haifeng, et al. Effect of indentation length of liquid-liquid coaxial swirling injector on spray process[J]. Journal of Rocket Propulsion, 2024, 50(3): 42-52. (in Chinese doi: 10.3969/j.issn.1672-9374.2024.03.005

    Wang Zhuang, Dang Xiaorui, Hu Haifeng, et al. Effect of indentation length of liquid-liquid coaxial swirling injector on spray process[J]. Journal of Rocket Propulsion, 2024, 50(3): 42-52. (in Chinese) doi: 10.3969/j.issn.1672-9374.2024.03.005
    [21]
    Natarajan V, Unnikrishnan U, Choi J Y, et al. Flow dynamics of a liquid-liquid bi-swirl injector[J]. Physics of Fluids, 2024, 36(3): 032122. doi: 10.1063/5.0191490
    [22]
    Hardalupas Y, Whitelaw J H. Interaction between sprays from multiple coaxial airblast atomizers[J]. Journal of Fluids Engineering, 1996, 118(4): 762-771. doi: 10.1115/1.2835507
    [23]
    侯燕, 陶毓伽, 淮秀兰. 多喷嘴喷雾场数值模拟分析[J]. 工程热物理学报, 2012, 33(8): 1362-1366. Hou Yan, Tao Yujia, Huai Xiulan. Numerical simulation and analysis of multi-nozzle spray cooling[J]. Journal of Engineering Thermophysics, 2012, 33(8): 1362-1366. (in Chinese

    Hou Yan, Tao Yujia, Huai Xiulan. Numerical simulation and analysis of multi-nozzle spray cooling[J]. Journal of Engineering Thermophysics, 2012, 33(8): 1362-1366. (in Chinese)
    [24]
    陈曦, 葛少成, 张忠温, 等. 基于Fluent多喷嘴喷雾干涉数值模拟分析[J]. 环境工程学报, 2014, 8(6): 2503-2508. Chen Xi, Ge Shaocheng, Zhang Zhongwen, et al. Numerical simulation and analysis of multi-nozzle interference base on Fluent[J]. Chinese Journal of Environmental Engineering, 2014, 8(6): 2503-2508. (in Chinese

    Chen Xi, Ge Shaocheng, Zhang Zhongwen, et al. Numerical simulation and analysis of multi-nozzle interference base on Fluent[J]. Chinese Journal of Environmental Engineering, 2014, 8(6): 2503-2508. (in Chinese)
    [25]
    王凯, 李鹏飞, 杨国华, 等. 相邻离心式喷嘴液膜撞击雾化过程仿真[J]. 推进技术, 2017, 38(2): 408-415. Wang Kai, Li Pengfei, Yang Guohua, et al. Simulation on liquid films impact atomization process of adjacent pressure swirl injectors[J]. Journal of Propulsion Technology, 2017, 38(2): 408-415. (in Chinese doi: 10.13675/j.cnki.tjjs.2017.02.020

    Wang Kai, Li Pengfei, Yang Guohua, et al. Simulation on liquid films impact atomization process of adjacent pressure swirl injectors[J]. Journal of Propulsion Technology, 2017, 38(2): 408-415. (in Chinese) doi: 10.13675/j.cnki.tjjs.2017.02.020
    [26]
    Song W, Koo J. Spray patterns of multi-element swirl coaxial injector of interacting spray under different injection conditions[J]. AIP Advances, 2021, 11(7): 075030. doi: 10.1063/5.0058107
    [27]
    康金鑫, 仝毅恒, 高玉超, 等. 同轴离心式单、双喷嘴喷雾特性对比实验[J]. 火箭推进, 2023, 49(6): 38-45. Kang Jinxin, Tong Yiheng, Gao Yuchao, et al. Comparative experimental of spray characteristics for gas liquid coaxial swirl single and double injectors[J]. Journal of Rocket Propulsion, 2023, 49(6): 38-45. (in Chinese

    Kang Jinxin, Tong Yiheng, Gao Yuchao, et al. Comparative experimental of spray characteristics for gas liquid coaxial swirl single and double injectors[J]. Journal of Rocket Propulsion, 2023, 49(6): 38-45. (in Chinese)
  • 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

    Article Metrics

    Article views (96) PDF downloads(14) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return