Comprehensive design method for lox/liquid-methane regenerative cooling combustor with coaxial injector

被引:0
|
作者
Yatsuyanagi, Nobuyuki [1 ]
机构
[1] Kakuda Research Center, National Aerospace Laboratory, Formerly, Kakuda, Japan
来源
Transactions of the Japan Society for Aeronautical and Space Sciences | 2009年 / 52卷 / 177期
关键词
Rocket engines;
D O I
暂无
中图分类号
学科分类号
摘要
Journal article (JA)
引用
收藏
页码:180 / 187
相关论文
共 45 条
  • [21] Near-field flow and flame dynamics of LOX/methane shear-coaxial injector under supercritical conditions
    Zong, Nan
    Yang, Vigor
    PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 : 2309 - 2317
  • [22] Longitudinal combustion instability in a hypergolic liquid bipropellant combustor with single dual-swirl coaxial injector
    Chu, Wei
    Guo, Kangkang
    Tong, Yiheng
    Ren, Yongjie
    Xu, Boqi
    Nie, Wansheng
    CHINESE JOURNAL OF AERONAUTICS, 2025, 38 (03)
  • [23] Numerical Simulation of Transcritical Liquid Film Cooling in LOX/Methane Liquid Rocket Engine Thrust Chambers
    Xiang J.-X.
    Zhang M.
    Li Z.-Q.
    Liu P.
    Wang H.
    Cui F.-J.
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (11): : 291 - 302
  • [24] Experimental Study on the Unsteady Spray Combustion Process of a Liquid Oxygen/Methane Swirl Coaxial Injector
    Cao, Pengjin
    Bai, Xiao
    Li, Qinglian
    Cheng, Peng
    Li, Ziguang
    ACS OMEGA, 2021, 6 (40): : 26191 - 26200
  • [25] Development of Preliminary Design Program for Combustor of Regenerative Cooled Liquid Rocket Engine
    Won Kook Cho
    Woo Seok Seol
    Min Son
    Min Kyo Seo
    Jaye Koo
    JournalofThermalScience, 2011, 20 (05) : 467 - 473
  • [26] Development of preliminary design program for combustor of regenerative cooled liquid rocket engine
    Won Kook Cho
    Woo Seok Seol
    Min Son
    Min Kyo Seo
    Jaye Koo
    Journal of Thermal Science, 2011, 20 : 467 - 473
  • [27] Development of Preliminary Design Program for Combustor of Regenerative Cooled Liquid Rocket Engine
    Cho, Won Kook
    Seol, Woo Seok
    Son, Min
    Seo, Min Kyo
    Koo, Jaye
    JOURNAL OF THERMAL SCIENCE, 2011, 20 (05) : 467 - 473
  • [28] Numerical study of combustion and cooling performance of a gaseous oxygen and gaseous methane rocket combustor with the needle-bolt injector
    Zhang, G. D.
    Li, G. X.
    Xing, R. P.
    Zhang, Hu
    Tang, G. H.
    APPLIED THERMAL ENGINEERING, 2023, 221
  • [29] Study on the design criteria of the coaxial injector for a LOX/hydrogen rocket engine -evaluation of design for injectors of the LE-5 engine and its derivatives
    Yatsuyanag, Nobuyuki
    Transactions of the Japan Society for Aeronautical and Space Sciences, 2007, 50 (169): : 201 - 208
  • [30] Study on the design criteria of the coaxial injector for a LOX/hydrogen rocket engine - Evaluation of design for injectors of the LE-5 engine and its derivatives
    Yatsuyanagi, Nobuyuki
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2007, 50 (169) : 201 - 208