Effect of equivalence ratio on kerosene-hydrogen-air rotating detonation propagation at room temperature

被引：0
|
作者：
Huang, Hanli [1 ]
Lyu, Yajin [2 ]
Zheng, Quan [1 ]
Wu, Mingliang [1 ]
Xiao, Qiang [1 ]
Wang, Fang [1 ]
Weng, Chunsheng [1 ]
机构：
[1] National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing,210094, China
[2] Shanghai Institute of Space Propulsion Research Center, Shanghai,201112, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2024年 / 39卷 / 09期
关键词：
D O I：
10.13224/j.cnki.jasp.20220712
中图分类号：
学科分类号：
摘要：
27
引用
收藏
相关论文
共 50 条
  • [31] Effects of the outlet contraction ratio on the performance of liquid kerosene/air two-phase rotating detonation combustors
    Li, Xiafei
    Jin, Wu
    Li, Jianzhong
    Yao, Qian
    Qin, Qiongyao
    Yuan, Li
    ACTA ASTRONAUTICA, 2024, 222 : 296 - 313
  • [32] Analysis of coupled-waves structure and propagation characteristics in hydrogen-assisted kerosene-air two-phase rotating detonation wave
    Huang, Xixuan
    Lin, Zhiyong
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2022, 47 (07) : 4868 - 4884
  • [33] Experimental research on the instability propagation characteristics of liquid kerosene rotating detonation wave
    Quan Zheng
    Hao-long Meng
    Chun-sheng Weng
    Yu-wen Wu
    Wen-kang Feng
    Ming-liang Wu
    Defence Technology, 2020, 16 (06) : 1106 - 1115
  • [34] Experimental Research on Initiation and Propagation Characteristics of Kerosene Fuel Rotating Detonation Wave
    Li B.
    Wang Z.
    Xu G.
    Weng C.
    Zhao F.
    Binggong Xuebao/Acta Armamentarii, 2020, 41 (07): : 1339 - 1346
  • [35] Experimental research on the instability propagation characteristics of liquid kerosene rotating detonation wave
    Zheng, Quan
    Meng, Hao-long
    Weng, Chun-sheng
    Wu, Yu-wen
    Feng, Wen-kang
    Wu, Ming-liang
    DEFENCE TECHNOLOGY, 2020, 16 (06) : 1106 - 1115
  • [36] Effect of inlet temperature and equivalence ratio on working process of pulse detonation engine
    Jiang, Tao
    Weng, Chun-Sheng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2015, 30 (01): : 29 - 37
  • [37] Numerical research on two-phase kerosene/air rotating detonation engines
    Wang, Fang
    Weng, Chunsheng
    ACTA ASTRONAUTICA, 2022, 192 : 199 - 209
  • [38] Propagation Stability of Rotating Detonation Waves Using Hydrogen/Oxygen-Enriched Air Mixtures
    Ikema, Daisuke
    Yokota, Atsushi
    Kurata, Wataru
    Kawana, Haruhiro
    Ishii, Kazuhiro
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2018, 61 (06) : 268 - 273
  • [39] Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics
    Zhou, Shengbing
    Ma, Hu
    Li, Shuai
    Liu, Daokun
    Yan, Yu
    Zhou, Changsheng
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2017, 42 (31) : 20297 - 20305
  • [40] Continuous spin detonation of a heterogeneous kerosene–air mixture with addition of hydrogen
    F. A. Bykovskii
    S. A. Zhdan
    E. F. Vedernikov
    Combustion, Explosion, and Shock Waves, 2016, 52 : 371 - 373
12345