Numerical study of turbulent reacting flows in solid-propellant ducted rocket combustors

被引:0
|
作者
机构
[1] Cherng, D.L.
[2] Yang, V.
[3] Kuo, K.K.
来源
Cherng, D.L. | 1600年 / 05期
关键词
Reacting Flows - Turbulent Mixing;
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 EXPERIMENTS ON THE DETERMINATION OF UNSTEADY STATE TEMPERATURE DISTRIBUTION IN A SOLID-PROPELLANT ROCKET MOTOR
    LAURA, PAA
    SARMIENTO, GS
    OLIVETTO, ME
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1979, 22 (04) : 625 - 628
  • [33] Multiscale Simulation of Gas-Particle Flows in the Combustion Chambers of Solid-Propellant Rocket Motors
    Brykov, N.
    Volkov, K.
    Emelyanov, V.
    Efremov, A.
    FLUID DYNAMICS, 2024, 59 (05) : 1416 - 1436
  • [34] Regularities of Physical Processes in Hybrid Solid-Propellant Rocket Engines
    S. S. Bondarchuk
    A. B. Vorozhtsov
    A. S. Zhukov
    B. V. Borisov
    Russian Physics Journal, 2015, 57 : 1796 - 1799
  • [35] COMPUTERIZED ULTRASONIC TOMOGRAPHY FOR TESTING SOLID-PROPELLANT ROCKET MOTORS
    SATTI, AMH
    SZILARD, J
    ULTRASONICS, 1983, 21 (04) : 162 - 166
  • [36] Discrimination for ablative control mechanism in solid-propellant rocket nozzle
    Huang HaiMing
    Xu XiaoLiang
    Jiang GuiQing
    SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2009, 52 (10): : 2911 - 2917
  • [37] ON SIMULATION OF COMBUSTION PROCESSES WITH LAGGING IN SOLID-PROPELLANT ROCKET ENGINE
    SHATALOV, YS
    DOZENKO, IN
    URAKAYEV, IM
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1991, (04): : 80 - 84
  • [38] MEASURED PARTICULATE BEHAVIOR IN A SUBSCALE SOLID-PROPELLANT ROCKET MOTOR
    BRENNAN, WD
    HOVLAND, DL
    NETZER, DW
    JOURNAL OF PROPULSION AND POWER, 1992, 8 (05) : 954 - 960
  • [39] REGULARITIES OF PHYSICAL PROCESSES IN HYBRID SOLID-PROPELLANT ROCKET ENGINES
    Bondarchuk, S. S.
    Vorozhtsov, A. B.
    Zhukov, A. S.
    Borisov, B. V.
    Russian Physics Journal, 2015, 57 (12) : 1796 - 1799
  • [40] Discrimination for ablative control mechanism in solid-propellant rocket nozzle
    HaiMing Huang
    XiaoLiang Xu
    GuiQing Jiang
    Science in China Series E: Technological Sciences, 2009, 52 : 2911 - 2917