Investigation on common nozzle of triple-tube pulse detonation engine with kerosene/air

被引:0
|
作者
Li, Jian-Zhong [1 ]
Wang, Jia-Hua [1 ]
Tang, Hao [1 ]
Pan, Bo [2 ]
机构
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
[2] PAL Headquarter of the General Staff Army Research Institute, Beijing 101114, China
来源
关键词
10;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:840 / 844
相关论文
共 50 条
  • [41] Experimental research on propulsive performance of the pulse detonation rocket engine with a fluidic nozzle
    Zhang, Qibin
    Wang, Ke
    Dong, Rongxiao
    Fan, Wei
    Lu, Wei
    Wang, Yongjia
    ENERGY, 2019, 166 : 1267 - 1275
  • [42] Experimental investigation of multi-cycle pulse detonation engine at different air inlet systems
    Ma, Hu
    Wu, Xiao-Song
    Wang, Dong
    Chen, Jun
    Feng, Feng
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2014, 228 (12) : 2207 - 2214
  • [43] Numerical investigation of multi-tube pulse detonation
    Ebrahimi, HB
    2003 USERS GROUP CONFERENCE, PROCEEDINGS, 2003, : 236 - 243
  • [44] Numerical investigation of flame propagation and performance of obstructed pulse detonation engine with variation of hydrogen and air
    Alam, Noor
    Sharma, K. K.
    Pandey, K. M.
    JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2019, 41 (11)
  • [45] Numerical investigation of flame propagation and performance of obstructed pulse detonation engine with variation of hydrogen and air
    Noor Alam
    K. K. Sharma
    K. M. Pandey
    Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2019, 41
  • [46] Numerical investigation of the ejector influence on the effectiveness of a jet nozzle of a detonation engine
    A. E. Korobov
    S. V. Golovastov
    High Temperature, 2015, 53 : 118 - 123
  • [47] Numerical investigation of the ejector influence on the effectiveness of a jet nozzle of a detonation engine
    Korobov, A. E.
    Golovastov, S. V.
    HIGH TEMPERATURE, 2015, 53 (01) : 118 - 123
  • [48] Preliminary Experimental Investigation on Detonation Initiation in the Ejector of a Pulse Detonation Rocket Engine
    Yan, Yu
    Fan, Wei
    Mu, Yang
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2012, 29 (04) : 299 - 307
  • [49] Experimental research on vector control features of a pulse detonation tube with fluidic nozzle
    Zhang, Qibin
    Wang, Ke
    Wang, Jigang
    Qiao, Xinqi
    Fan, Wei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 116
  • [50] Experimental investigation on valveless air-breathing dual-tube pulse detonation engines
    Peng, Changxin
    Fan, Wei
    Zheng, Longxi
    Wang, Zhiwu
    Yuan, Cheng
    APPLIED THERMAL ENGINEERING, 2013, 51 (1-2) : 1116 - 1123