Numerical simulation and experimental investigation on binary mixed-compression supersonic inlet

被引：0
|
作者：
Dong, Jia-Feng [1 ,2 ]
Li, Jin-Xian [1 ]
Cui, Jin-Ping [2 ]
Cao, Jun-Wei [2 ]
Wang, Hu-Gan [2 ]
机构：
[1] College of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
[2] China Airborne Missile Academy, Luoyang 471009, China
来源：
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2008年 / 31卷 / 02期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
6
引用
收藏
页码：129 / 132
相关论文
共 50 条
  • [1] NUMERICAL INVESTIGATION OF SUPERSONIC MIXED-COMPRESSION INLET USING AN IMPLICIT UPWIND SCHEME
    CHAN, JJ
    LIANG, SM
    JOURNAL OF PROPULSION AND POWER, 1992, 8 (01) : 158 - 167
  • [2] Euler flow in a supersonic mixed-compression inlet
    Jain, MK
    Mittal, S
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2006, 50 (12) : 1405 - 1423
  • [3] Numerical simulation and experimental investigation on mixed-compression inlet of solid fuel ramjet extended-range projectile
    Xia, Qiang
    Wu, Xiao-Song
    Sun, Bo
    Xiong, Zhi-Ping
    Binggong Xuebao/Acta Armamentarii, 2010, 31 (10): : 1372 - 1378
  • [4] Experimental Investigation on Mixed-Compression Inlet of Solid Fuel Ramjet Projectile
    Sun, Bo
    Wu, Xiaosong
    Xia, Qiang
    Yu, Ling
    Cai, Wenxiang
    PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING AND MECHANICS, VOLS 1 AND 2, 2009, : 224 - 227
  • [5] Numerical Vibration Analysis of Supersonic Mixed-Compression Intake
    Cheng, Yao
    Liu, Zhansheng
    Ma, Ruixian
    Zhang, Guanghui
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 2, 2013,
  • [6] Numerical analysis on three-dimensional flow in 2-D mixed-compression supersonic inlet
    Wang, G.H.
    Li, J.X.
    Cai, T.M.
    Tuijin Jishu/Journal of Propulsion Technology, 2001, 22 (02): : 118 - 121
  • [7] Design of a two-dimensional mixed-compression supersonic inlet with boundary layer consideration
    Luo, Guang-Qi
    Zheng, Jiu-Zhou
    Song, Di-Yuan
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (09): : 2063 - 2068
  • [8] BLEED BOUNDARY-CONDITIONS FOR NUMERICALLY SIMULATED MIXED-COMPRESSION SUPERSONIC INLET FLOW
    CHYU, WJ
    HOWE, GW
    SHIH, TIP
    JOURNAL OF PROPULSION AND POWER, 1992, 8 (04) : 862 - 868
  • [9] Flow response hysteresis of throat regulation process of a two-dimensional mixed-compression supersonic inlet
    Jin, Yi
    Sun, Shu
    Tan, Huijun
    Zhang, Yue
    Huang, Hexia
    CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (03) : 112 - 127
  • [10] EXPERIMENTAL INVESTIGATION OF TERMINAL SHOCK SENSORS FOR MIXED-COMPRESSION INLETS
    SAJBEN, M
    DONOVAN, JF
    MORRIS, MJ
    JOURNAL OF PROPULSION AND POWER, 1992, 8 (01) : 168 - 174
12345