Numerical investigation on propagation behavior of gaseous detonation in water spray

被引:29
|
作者
Watanabe, Hiroaki [1 ]
Matsuo, Akiko [1 ]
Matsuoka, Ken [2 ]
Kawasaki, Akira [2 ]
Kasahara, Jiro [2 ]
机构
[1] Keio Univ, Dept Mech Engn, Kohoku Ku, 3-14-1 Hiyoshi, Yokohama, Kanagawa 2238522, Japan
[2] Nagoya Univ, Dept Aerosp Engn, Chikusa Ku, Furo Cho, Nagoya, Aichi 4648603, Japan
关键词
Detonation; Water droplet; Evaporation; Average structure; Velocity decrease; MODEL; COMBUSTION; PROPULSION;
D O I
10.1016/j.proci.2018.07.092
中图分类号
O414.1 [热力学];
学科分类号
摘要
A two-dimensional (2D) numerical simulation is conducted to clarify the propagation behavior of gaseous detonation in a water spray and its structure. The computational target refers to the experiment conducted by G Jarsale et al., and C2H4 -air gaseous detonation propagates where the water droplets (WDs) are sprayed. The parameters used are the C2H4-air equivalence ratio and WD mass fraction. The flow field, Favre-averaged one-dimensional profile, and cellular structure are revealed in 2D simulations. Stable propagation of gaseous detonation is observed in the water spray, and the decrease in velocity relative to the Chapman-Jouguet velocity without WDs is as much as 3.2%. Adding WDs changes the cellular pattern, especially for leaner mixtures. The weak triple point decays. and the cell width increases because of the longer induction length due to decreased velocity. The WD presence changes the detonation flow field substantially, and evaporation occurs primarily at 10 mm behind the shock wave. The high-evaporation region propagates at the detonation speed, and the compression wave formed when the detonation reflects from the two-phase medium propagates backward. Furthermore, WD evaporation suppresses the velocity, vorticity, and temperature fluctuations. Rapid evaporation with WDs leads to lower hydrodynamic thickness than that without WDs or in the Zel'dovich-von Neumann-Doring model. (C) 2018 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:3617 / 3626
页数:10
相关论文
共 50 条
  • [1] Numerical analysis of the mean structure of gaseous detonation with dilute water spray
    Watanabe, Hiroaki
    Matsuo, Akiko
    Chinnayya, Ashwin
    Matsuoka, Ken
    Kawasaki, Akira
    Kasahara, Jiro
    JOURNAL OF FLUID MECHANICS, 2020, 887
  • [2] Numerical investigation on gaseous detonation diffraction
    Li, Hai-Peng
    He, Li-Ming
    Luo, Jun
    Zeng, Hao
    Wu, Wei
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2010, 25 (03): : 496 - 502
  • [3] Numerical investigation on the interaction characteristics between the gaseous detonation wave and the water droplet
    Xu, Sheng
    Jin, Xin
    Fan, Wenqi
    Wen, Haocheng
    Wang, Bing
    COMBUSTION AND FLAME, 2024, 269
  • [4] Numerical Study of Spray Combustion Effects on Detonation Propagation
    Salvadori, Marc
    Panchal, Achyut
    Menon, Suresh
    AIAA JOURNAL, 2023, 61 (12) : 5347 - 5364
  • [5] Numerical Simulations of Gaseous Detonation Propagation Using Different Supercomputing Architechtures
    Smirnov, N. N.
    Nikitin, V. F.
    Stamov, L. I.
    Nerchenko, V. A.
    Tyrenkova, V. V.
    INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2017, 14 (04)
  • [6] Numerical Simulation of Gaseous Detonation Propagation in a Multi-Tube Device
    Wang Changjian
    Guo Changming
    THEORY AND PRACTICE OF ENERGETIC MATERIALS, VOL VIII, 2009, : 537 - 541
  • [7] Experimental and Numerical Investigation of Gaseous Detonation in a Narrow Channel with Obstacles
    Krivosheyev, Pavel N.
    Novitski, Alexey O.
    Sevrouk, Kirill L.
    Penyazkov, Oleg G.
    But, Ivan I.
    Kasimov, Aslan R.
    FLUIDS, 2021, 6 (06)
  • [8] Investigation of the propagation modes for gaseous detonation at near-limit condition
    Yan B.
    Zhang B.
    Gao Y.
    Lyu S.
    Zhang, Bo (zhangb@live.cn), 2018, Explosion and Shock Waves (38): : 1435 - 1440
  • [9] Numerical investigation of detonation combustion wave propagation in pulse detonation combustor with nozzle
    Debnath, Pinku
    Pandey, K. M.
    ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, 2020, 7 (03): : 187 - 202
  • [10] Schlieren visualization and numerical simulation on gaseous detonation propagation through a bend tube
    Department of Mechanics and Mechanical Engineering, University of Science and Technology of China, Hefei 230026, China
    不详
    Lixue Xuebao, 2006, 1 (9-15):