Propulsive performance of pulse detonation engine with fluidically augmented nozzle

被引：0
|
作者：
机构：
[1] Zheng, Hua-Lei
[2] Qiu, Hua
[3] Xiong, Cha
[4] Zheng, Long-Xi
来源：
Zheng, H.-L. (008zheng@163.com) | 1600年 / Journal of Propulsion Technology卷 / 35期
关键词：
Combustion;
D O I：
10.13675/j.cnki.tjjs.2014.07.018
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] Calculation and analysis of pulse detonation engine flight performance
    Engineering Inst., Air Force Engineering Univ., Xi'an 710038, China
    Tuijin Jishu, 2007, 2 (190-193):
  • [32] Effect of operation frequency on pulse detonation engine performance
    Huang, Xiqiao
    Yan, Chuanjun
    Wang, Zhiwu
    Fan, Wei
    Jiang, Bo
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2007, 25 (01): : 22 - 26
  • [33] Review on Factors Affecting the Performance of pulse Detonation Engine
    Tripathi, Saurabh
    Pandey, Krishna Murari
    INTERNATIONAL CONFERENCE ON ELECTRICAL, ELECTRONICS, MATERIALS AND APPLIED SCIENCE, 2018, 1952
  • [34] Nozzle Design for Rotating Detonation Engine
    Li, Rui
    Xu, Jinglei
    Huang, Shuai
    JOURNAL OF PROPULSION AND POWER, 2022, 38 (05) : 849 - 865
  • [35] Numerical simulation of the effects of nozzle on thrust performance of rotating detonation engine
    Eto, Seiichiro
    Watanabe, Yusuke
    Tsuboi, Nobuyuki
    Kojima, Takayuki
    Hayashi, A. Koichi
    SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS, 2016, 77 (5-6) : 122 - 127
  • [36] Experimental study of the influence of annular nozzle on acoustic characteristics of detonation sound wave generated by pulse detonation engine
    Kang, Yang
    Li, Ning
    Huang, Xiao-Long
    Weng, Chun-Sheng
    CHINESE PHYSICS B, 2022, 31 (10)
  • [37] Experimental study of the influence of annular nozzle on acoustic characteristics of detonation sound wave generated by pulse detonation engine
    康杨
    李宁
    黄孝龙
    翁春生
    Chinese Physics B, 2022, 31 (10) : 503 - 510
  • [38] Oxygen concentration distribution in a pulse detonation engine with nozzle-ejector combinational structures
    Wang, Zhiwu
    Wei, Lisi
    Qin, Weifeng
    Liang, Zijian
    Zhang, Kun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2021, 235 (14) : 2059 - 2068
  • [39] Investigation on common nozzle of triple-tube pulse detonation engine with kerosene/air
    Li, Jian-Zhong
    Wang, Jia-Hua
    Tang, Hao
    Pan, Bo
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2008, 23 (05): : 840 - 844
  • [40] Numerical simulation of converging-diverging nozzle flow in pulse detonation rocket engine
    School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
    Beijing Hangkong Hangtian Daxue Xuebao, 2007, 7 (789-792):
12345