Study on numerical simulations of a plug nozzle for rocket engine

被引:0
|
作者
Zhuge, Weilin
Zhang, Yangjun
Ma, Jihua
Zhang, Zhenpeng
机构
来源
Yuhang Xuebao/Journal of Astronautics | 1999年 / 20卷 / 04期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
下载
收藏
页码:18 / 24
相关论文
共 50 条
  • [1] Numerical simulations on RBCC engine in Scramjet/rocket mode
    Tang, Xiang
    He, Guo-Qiang
    Qin, Fei
    Tuijin Jishu/Journal of Propulsion Technology, 2013, 34 (12): : 1643 - 1649
  • [2] Numerical study of the hybrid rocket engine
    C. Ommounica
    Sachin Srivastava
    Subham Haldar
    Aerospace Systems, 2025, 8 (1) : 237 - 245
  • [3] Experimental Testing and Numerical Simulations of Shrouded Plug-Nozzle Flowfields
    Kapilavai, Dheeraj S. K.
    Tapee, John
    Sullivan, John
    Merkle, Charles L.
    Wayman, Thomas R.
    Conners, Timothy R.
    JOURNAL OF PROPULSION AND POWER, 2012, 28 (03) : 530 - 544
  • [4] Electrification of Nozzle in a Liquid Rocket Engine
    Yagodnikov, D. A.
    Voronetskii, A. V.
    Pushkin, N. M.
    Combustion, Explosion, and Shock Waves, 31 (04):
  • [5] Electrification of nozzle in a liquid rocket engine
    Yagodnikov, DA
    Voronetskii, AV
    Pushkin, NM
    COMBUSTION EXPLOSION AND SHOCK WAVES, 1995, 31 (04) : 450 - 454
  • [6] Numerical Simulation of Tail Flow Field of Four - Nozzle Solid Rocket Engine
    Zha, Bailin
    Hui, Zhe
    Su, Qingdong
    2018 2ND INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND INDUSTRIAL APPLICATIONS, 2018, 1064
  • [7] Numerical simulation of fluid–structure interaction for solid rocket engine nozzle ablation
    Donghui Wang
    Dehua Cao
    Zhitan Zhou
    Ranhui Liang
    Advances in Aerodynamics, 2025, 7 (1)
  • [8] Numerical study of the aeroelastic stability of an overexpanded rocket nozzle
    Lefrançois, Emmanuel
    Dhatt, Gouri
    Vandromme, Dany
    Revue Europeenne des Elements, 2000, 9 (6-7): : 727 - 762
  • [9] Trihybrid nanofluid flow through nozzle of a rocket engine: Numerical solution and irreversibility analysis
    Ullah, Basharat
    Rehman, Rabia
    Wahab, Hafiz Abdul
    Khan, Umar
    Emam, Walid
    ENERGY EXPLORATION & EXPLOITATION, 2024, : 302 - 318
  • [10] 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):