Volume 40 Issue 9
Sep.  2025
Turn off MathJax
Article Contents
CHEN Qingyun, ZHANG Qibin, YANG Rui, et al. Numerical study on breakup, evaporation, and combustion characteristics of kerosene droplets under detonation waves[J]. Journal of Aerospace Power, 2025, 40(9):20240377 doi: 10.13224/j.cnki.jasp.20240377
Citation: CHEN Qingyun, ZHANG Qibin, YANG Rui, et al. Numerical study on breakup, evaporation, and combustion characteristics of kerosene droplets under detonation waves[J]. Journal of Aerospace Power, 2025, 40(9):20240377 doi: 10.13224/j.cnki.jasp.20240377

Numerical study on breakup, evaporation, and combustion characteristics of kerosene droplets under detonation waves

doi: 10.13224/j.cnki.jasp.20240377
  • Received Date: 2024-06-11
    Available Online: 2024-12-04
  • Numerical investigation was conducted with VOF (volume of fluid) multiphase flow model and RNG (re-normalization group) k-ε turbulence model to explore the effects of detonation waves on the breakup, evaporation, and combustion characteristics of RP-3 kerosene droplets. Through adjusting the initial pressures (20, 30, 40 kPa) under different equivalence ratios (0.8 to 1.2), the evolution of the droplet breakup morphology, characteristics of evaporation, and flame shape were obtained. The results indicated that, under the detonation wave, the main stages of the evolution of RP-3 kerosene droplet breakup can be categorized into the wrinkling, squeezing, development, and the stable period according to the characteristics of the droplet morphology. The evaporation characteristics of the droplet were relatively less influenced by the Weber number, the linear relationship between windward displacement S and We was fitted, with the liquid phase mass fraction remaining within the range of 41% to 56% before the break-up morphological profile was stabilized. The liquid-phase evaporation rate increased over time and then gradually decreased. As the Weber number increased, the rate of displacement growth on the windward side of the droplet decreased, while the rate of flattening accelerated. During the combustion process, the "pinch" flame became more compact and penetrated deeper. The size and curvature of the swirling flame also gradually increased, and irregular fully enveloping flame shapes became more complex.

     

  • loading
  • [1]
    KAILASANATH K. Recent developments in the research on pulse detonation engines[J]. AIAA Journal, 2003, 41(2): 145-159. doi: 10.2514/2.1933
    [2]
    严传俊, 范玮. 脉冲爆震发动机原理及关键技术[M]. 西安: 西北工业大学出版社, 2005. YAN Chuanjun, FAN Wei. Principle and key technology of pulse detonation engine[M]. Xi’an: Northwestern Polytechnical University Press, 2005. (in Chinese

    YAN Chuanjun, FAN Wei. Principle and key technology of pulse detonation engine[M]. Xi’an: Northwestern Polytechnical University Press, 2005. (in Chinese)
    [3]
    CALDWELL N, GLASER A, GUTMARK E. A review of pulse detonation engine research at the University of Cincinnati: AIAA2007-5697 [R]. Reston, US: AIAA, 2007.
    [4]
    KAILASANATH K. Review of propulsion applications of detonation waves[J]. AIAA Journal, 2000, 38(9): 1698-1708. doi: 10.2514/2.1156
    [5]
    WANG Ke, FAN Wei, LU Wei, et al. Study on a liquid-fueled and valveless pulse detonation rocket engine without the purge process[J]. Energy, 2014, 71: 605-614. doi: 10.1016/j.energy.2014.05.002
    [6]
    SUN Jian, ZHOU Jin, LIU Shijie, et al. Numerical investigation of a rotating detonation engine under premixed/non-premixed conditions[J]. Acta Astronautica, 2018, 152: 630-638. doi: 10.1016/j.actaastro.2018.09.012
    [7]
    WATANABE H, MATSUO A, MATSUOKA K, et al. Numerical investigation on propagation behavior of gaseous detonation in water spray[J]. Proceedings of the Combustion Institute, 2019, 37(3): 3617-3626. doi: 10.1016/j.proci.2018.07.092
    [8]
    WEN Haocheng, WEI Wei, FAN Wenqi, et al. On the propagation stability of droplet-laden two-phase rotating detonation waves[J]. Combustion and Flame, 2022, 244: 112271. doi: 10.1016/j.combustflame.2022.112271
    [9]
    PILCH M, ERDMAN C A. Use of breakup time data and velocity history data to predict the maximum size of stable fragments for acceleration-induced breakup of a liquid drop[J]. International Journal of Multiphase Flow, 1987, 13(6): 741-757. doi: 10.1016/0301-9322(87)90063-2
    [10]
    YOSHIDA T, NAGAI N. A study of the critical conditions for the breakup of a liquid droplet by air streams[J]. Transactions of the Japan Society of Mechanical Engineers: Series B, 1986, 52(475): 1363-1371. doi: 10.1299/kikaib.52.1363
    [11]
    肖毅, 施红辉, 吴宇, 等. 激波与液滴作用的空气动力学现象的实验研究[J]. 浙江理工大学学报, 2013, 30(2): 203-207. XIAO Yi, SHI Honghui, WU Yu, et al. Experimental study on aerodynamic phenomenon of interaction between shock wave and liquid drop[J]. Journal of Zhejiang Sci-Tech University (Natural Sciences Edition), 2013, 30(2): 203-207. (in Chinese doi: 10.3969/j.issn.1673-3851.2013.02.015

    XIAO Yi, SHI Honghui, WU Yu, et al. Experimental study on aerodynamic phenomenon of interaction between shock wave and liquid drop[J]. Journal of Zhejiang Sci-Tech University (Natural Sciences Edition), 2013, 30(2): 203-207. (in Chinese) doi: 10.3969/j.issn.1673-3851.2013.02.015
    [12]
    刘晨. 超声速条件下液滴动力学特性研究[D]. 杭州: 浙江理工大学, 2019. LIU Chen. Study on dynamic characteristics of droplets at supersonic velocity[D]. Hangzhou: Zhejiang Sci-Tech University, 2019. (in Chinese

    LIU Chen. Study on dynamic characteristics of droplets at supersonic velocity[D]. Hangzhou: Zhejiang Sci-Tech University, 2019. (in Chinese)
    [13]
    施红辉, 刘晨, 熊红平, 等. 激波冲击下液滴变形破碎的黏性特征[J]. 航空动力学报, 2019, 34(9): 1962-1970. SHI Honghui, LIU Chen, XIONG Hongping, et al. Viscosity characteristics of droplet deformation and breakup under shock wave[J]. Journal of Aerospace Power, 2019, 34(9): 1962-1970. (in Chinese

    SHI Honghui, LIU Chen, XIONG Hongping, et al. Viscosity characteristics of droplet deformation and breakup under shock wave[J]. Journal of Aerospace Power, 2019, 34(9): 1962-1970. (in Chinese)
    [14]
    申帅. 激波作用下燃油液滴变形破碎行为和机理研究[D]. 西安: 西北工业大学, 2021. SHEN Shuai. Investigations on the droples deformation and breakup behaviors and mechanism of fuel droplet under the action of a shock wave[D]. Xi’an: Northwestern Polytechnical University, 2021. (in Chinese

    SHEN Shuai. Investigations on the droples deformation and breakup behaviors and mechanism of fuel droplet under the action of a shock wave[D]. Xi’an: Northwestern Polytechnical University, 2021. (in Chinese)
    [15]
    SALAUDDIN S, MORALES A J, HYTOVICK R, et al. Detonation and shock-induced breakup characteristics of RP-2 liquid droplets[J]. Shock Waves, 2023, 33(3): 191-203. doi: 10.1007/s00193-023-01132-7
    [16]
    宋家喜, 潘书诚. 高马赫数下激波液滴相互作用的数值模拟研究[J]. 力学学报, 2022, 54(9): 2419-2434. SONG Jiaxi, PAN Shucheng. Numerical investigation of shock-droplet interaction with high-Mach numbers[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(9): 2419-2434. (in Chinese doi: 10.6052/0459-1879-22-191

    SONG Jiaxi, PAN Shucheng. Numerical investigation of shock-droplet interaction with high-Mach numbers[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(9): 2419-2434. (in Chinese) doi: 10.6052/0459-1879-22-191
    [17]
    LI Jianghong, LEI Ying, YAO Songbai, et al. Investigation of multi-stage evaporation and wave multiplicity of two-phase rotating detonation waves fueled by ethanol[J]. Acta Astronautica, 2023, 213: 418-430. doi: 10.1016/j.actaastro.2023.08.037
    [18]
    MUSICK B J, PAUDEL M, RAMAPRABHU P K, et al. Numerical simulations of droplet evaporation and breakup effects on heterogeneous detonations[J]. Combustion and Flame, 2023, 257: 113035. doi: 10.1016/j.combustflame.2023.113035
    [19]
    李科, 赵钰祥, 武文斐. 单油滴蒸发燃烧周围流场及火焰结构的数值模拟研究[J]. 热科学与技术, 2015, 14(3): 178-183. LI Ke, ZHAO Yuxiang, WU Wenfei. Numerical study on surrounding gas flow and flame structures of single combusting droplet[J]. Journal of Thermal Science and Technology, 2015, 14(3): 178-183. (in Chinese

    LI Ke, ZHAO Yuxiang, WU Wenfei. Numerical study on surrounding gas flow and flame structures of single combusting droplet[J]. Journal of Thermal Science and Technology, 2015, 14(3): 178-183. (in Chinese)
    [20]
    MERCIER X, ORAIN M, GRISCH F. Investigation of droplet combustion in strained counterflow diffusion flames using planar laser-induced fluorescence[J]. Applied Physics: B, 2007, 88(1): 151-160. doi: 10.1007/s00340-007-2605-y
    [21]
    施红辉, 章易鑫, 师顺, 等. 激波与亚毫米液滴相互作用的二维和三维数值模拟研究[J]. 过程工程学报, 2022, 22(8): 1061-1073. SHI Honghui, ZHANG Yixin, SHI Shun, et al. 2D and 3D numerical study on the interaction of shock wave and sub-millimeter water droplet[J]. The Chinese Journal of Process Engineering, 2022, 22(8): 1061-1073. (in Chinese doi: 10.12034/j.issn.1009-606X.221240

    SHI Honghui, ZHANG Yixin, SHI Shun, et al. 2D and 3D numerical study on the interaction of shock wave and sub-millimeter water droplet[J]. The Chinese Journal of Process Engineering, 2022, 22(8): 1061-1073. (in Chinese) doi: 10.12034/j.issn.1009-606X.221240
    [22]
    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
    [23]
    LEE W H. A pressure iteration scheme for two-phase flow modelling [M]. Washington, US: Hemisphere Publishing, 1980.
    [24]
    宋光辉. 气相作用下液滴形态演变过程研究[D]. 西安: 西安石油大学, 2021. SONG Guanghui. Study on the evolution process of droplet morphology under the action of gas phase[D]. Xi’an: Xi’an Shiyou University, 2021. (in Chinese

    SONG Guanghui. Study on the evolution process of droplet morphology under the action of gas phase[D]. Xi’an: Xi’an Shiyou University, 2021. (in Chinese)
    [25]
    陈伟威. 基于RNG k-ε紊流模型的溢洪道水力特性数值模拟[J]. 水利科学与寒区工程, 2023, 6(1): 10-13. CHEN Weiwei. Numerical simulation of hydraulic characteristics of spillway based on RNG k-ε turbulence model[J]. Hydro Science and Cold Zone Engineering, 2023, 6(1): 10-13. (in Chinese doi: 10.3969/j.issn.2096-5419.2023.01.004

    CHEN Weiwei. Numerical simulation of hydraulic characteristics of spillway based on RNG k-ε turbulence model[J]. Hydro Science and Cold Zone Engineering, 2023, 6(1): 10-13. (in Chinese) doi: 10.3969/j.issn.2096-5419.2023.01.004
    [26]
    THEOFANOUS T G. Aero breakup of Newtonian and viscoelastic liquids[J]. Annual Review of Fluid Mechanics, 2011, 43: 661-690. doi: 10.1146/annurev-fluid-122109-160638
    [27]
    THEOFANOUS T G, LI G J. On the physics of aerobreakup[J]. Physics of Fluids, 2008, 20(5): 10706631.
    [28]
    TAYLOR G. The instability of liquid surfaces when accelerated in a direction perpendicular to their planes: Ⅰ[J]. Proceedings of the Royal Society of London: Series A Mathematical and Physical Sciences, 1950, 201(1065): 192-196.
    [29]
    HUANG Xixuan, LIN Zhiyong. Study of the mechanism of shock-induced and detonation-induced droplet breakup based on hybrid solvers[J]. Physics of Fluids, 2024, 36(8): 086102. doi: 10.1063/5.0218526
  • 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 (687) PDF downloads(57) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return