Analysis of unsteady deposition process in the secondary combustion chamber of solid rocket ramjet

被引：0
|
作者：
Wang, De-Quan [1 ]
Xia, Zhi-Xun [1 ]
Hu, Jian-Xin [1 ]
机构：
[1] Institution of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2011年 / 34卷 / 01期
关键词：
Big particles - Deposition distribution - Deposition process - Flow boundaries - Groove effects - High temperature - Initial stages - Internal walls - Moving mesh - Secondary combustion chamber - Small particles - Solid rocket ramjet - Stochastic trajectory models - Unsteady deposition;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：48 / 51
相关论文
共 50 条
  • [31] Velocities of reacting boron particles within a solid fuel ramjet combustion chamber
    Sender, J
    Ciezki, HK
    DEFENCE SCIENCE JOURNAL, 1998, 48 (04) : 343 - 349
  • [32] Influence of Twice Air-entering on the Combustion and Ablation Environment of Solid Rocket Ramjet
    Wen Y.
    Wang J.
    Zha B.
    Xu Z.
    Binggong Xuebao/Acta Armamentarii, 2022, 43 (04): : 804 - 813
  • [33] Experimental and Numerical Studies on Fuel Injection and Combustion of Solid-Liquid Rocket Ramjet
    Lin Zhen
    Yang Wenjiang
    Qin Lizi
    Liu Yu
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 1180 - 1183
  • [34] FLOWFIELD IN COMBUSTION CHAMBER OF A SOLID-PROPELLANT ROCKET MOTOR
    DUNLAP, R
    WILLOUGH.PG
    HERMSEN, RW
    AIAA JOURNAL, 1974, 12 (10) : 1440 - 1442
  • [35] Influence of after-burning chamber dome length on secondary combustion for solid ducted rocket motor
    Jin, Bing-Le (jinbingle@nwpu.edu.cn), 1600, International Astronautical Federation, IAF (00):
  • [36] Test method of combustion efficiency for condensed products of boron-based propellant in secondary combustion chamber of solid ducted rocket
    Wu, Q. (wuqiu215@163.com), 1600, Journal of Solid Rocket Technology (37):
  • [37] Conceptual analysis of rocket dual combustion ramjet combined-cycle engine
    Wu J.
    Tan J.
    Chen J.
    Zhang Z.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2019, 41 (05): : 8 - 15
  • [38] Low-frequency acoustic instability of the working process in the combustion chamber of the solid propellant rocket engine
    Davydov, Yu. M.
    Egorov, M. Yu.
    JOURNAL OF VIBROENGINEERING, 2008, 10 (02) : 155 - 164
  • [39] Influence of recessing nozzle extent on a process of heat exchange in the combustion chamber of a solid fuel rocket engine
    Benderskyi, B. Ya
    Chernova, A. A.
    XXXVI SIBERIAN THERMOPHYSICAL SEMINAR (STS 36), 2020, 1677
  • [40] Influence of a flight overload on instability of working process in the combustion chamber of the solid-fuel rocket motor
    Davydov, Yu.M.
    Davydova, I.M.
    Egorov, M.Yu.
    Doklady Akademii Nauk, 2004, 398 (02) : 194 - 197
12345