Dynamics models for the combustor component in liquid rocket engine

被引：0
|
作者：
Liu, Shang [1 ]
Liu, Hong-Jun [1 ]
Chen, Hong-Yu [1 ]
机构：
[1] Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2012年 / 33卷 / 10期
关键词：
Combustors;
D O I：
10.3873/j.issn.1000-1328.2012.10.022
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1512 / 1518
相关论文
共 50 条
  • [41] Dynamical systems approach to study thermoacoustic transitions in a liquid rocket combustor
    Kasthuri, Praveen
    Pavithran, Induja
    Pawar, Samadhan A.
    Sujith, R. I.
    Gejji, Rohan
    Anderson, William
    CHAOS, 2019, 29 (10)
  • [42] Interaction of acoustic pressure and heat release rate fluctuations in a model rocket engine combustor
    Ueta, Riko
    Gotoda, Hiroshi
    Okamoto, Hirotaka
    Kawano, Kazuki
    Shoji, Takeshi
    Yoshida, Seiji
    PHYSICAL REVIEW E, 2024, 110 (01)
  • [43] Conceptual Design of a Supercritical Oxyfuel Combustor Based on LOX/Methane Rocket Engine Technologies
    Chowdhury, A. S. M. Arifur
    Badhani, Antara
    Cabrera, Luisa
    Choudhuri, Ahsan
    Love, Noonan D.
    14TH INTERNATIONAL ENERGY CONVERSION ENGINEERING CONFERENCE, 2016,
  • [44] High frequency combustion instability control by discharge plasma in a model rocket engine combustor
    Zhou, Siyin
    Nie, Wansheng
    Tian, Yuan
    ACTA ASTRONAUTICA, 2021, 179 : 391 - 406
  • [45] High frequency combustion instability control by discharge plasma in a model rocket engine combustor
    Zhou, Siyin
    Nie, Wansheng
    Tian, Yuan
    Zhou, Siyin (siyin_zhou@126.com); Nie, Wansheng (nws1969@126.com), 1600, Elsevier Ltd (179): : 391 - 406
  • [46] DYNAMICS OF A LIQUID ROCKET SYSTEM - COMMENTS
    SANDERS, JC
    JET PROPULSION, 1957, 27 (04): : 421 - 421
  • [47] Rocket Engine with Continuous Film Detonation of Liquid Fuel
    S. M. Frolov
    I. O. Shamshin
    V. S. Aksenov
    I. A. Sadykov
    P. A. Gusev
    V. A. Zelenskii
    E. V. Evstratov
    M. I. Alymov
    Doklady Physical Chemistry, 2018, 481 : 105 - 109
  • [48] Formation mechanism of high-frequency combustion oscillations in a model rocket engine combustor
    Shima, Satomi
    Nakamura, Kosuke
    Gotoda, Hiroshi
    Ohmichi, Yuya
    Matsuyama, Shingo
    PHYSICS OF FLUIDS, 2021, 33 (06)
  • [49] Stabilizing liquid-propellant rocket engine operation
    Bajramov, F.D.
    Izvestiya VUZ: Aviatsionnaya Tekhnika, 1991, (01): : 37 - 42
  • [50] Development of a system analysis program for a liquid rocket engine
    Sangbok Lee
    Taekyu Lim
    Tae-Seong Roh
    Journal of Mechanical Science and Technology, 2015, 29 : 2375 - 2380
12345