Numerical analysis of acoustical wave-motion in combustion chamber of liquid rocket engine

被引:0
|
作者
Shanghai Jiaotong Univ, Shanghai, China [1 ]
机构
来源
Tuijin Jishu | / 2卷 / 5-8期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [31] Numerical simulation of combustion stability of liquid rocket engine based on chemistry dynamics
    Huang, YH
    Wang, ZG
    Zhou, J
    SCIENCE IN CHINA SERIES B-CHEMISTRY, 2002, 45 (05): : 551 - U1
  • [32] A numerical study of combustion and heat transfer in small thrust liquid rocket engine
    Lin, Qingguo
    Zhou, Jin
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2012, 34 (04): : 13 - 17
  • [33] Numerical simulation of combustion stability of liquid rocket engine based on chemistry dynamics
    Yuhui Huang
    Zhenguo Wang
    Jin Zhou
    Science in China Series B: Chemistry, 2002, 45 : 551 - 560
  • [34] Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine
    Qin, Jianxiu
    Zhang, Huiqiang
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, 2020 (2020)
  • [35] Numerical simulation of three-dimensional flow in combustion chamber of solid propellant rocket engine
    Mei, Liquan
    Huang, Qinghuai
    Ranshao Kexue Yu Jishu/Journal of Combustion Science and Technology, 1996, 2 (03): : 256 - 259
  • [37] Simulation of Liquid Fuel Combustion of a Rocket Engine
    Seralathan S.
    Sandeep K.
    Ejaz Z.H.
    Sufiyan S.
    Hariram V.
    Paul R.C.
    Nadanakumar V.
    International Journal of Vehicle Structures and Systems, 2022, 14 (06) : 820 - 825
  • [38] Numerical investigations of thermal stratification in cooling channel of liquid rocket engine thrust chamber
    School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100091, China
    不详
    Hangkong Dongli Xuebao, 2009, 8 (1904-1910):
  • [39] Remaining Useful Life Prediction with Uncertainty Quantification of Liquid Propulsion Rocket Engine Combustion Chamber
    Kanso, Soha
    Jha, Mayank S.
    Galeotta, Marco
    Theilliol, Didier
    IFAC PAPERSONLINE, 2022, 55 (06): : 96 - 101
  • [40] Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine
    Zarubin V.S.
    Zimin V.N.
    Kuvyrkin G.N.
    Russian Aeronautics, 2018, 61 (03): : 425 - 433