Numerical analysis on three-dimensional flow in 2-D mixed-compression supersonic inlet

被引：0
|
作者：
Wang, G.H. [1 ]
Li, J.X. [1 ]
Cai, T.M. [1 ]
机构：
[1] Coll. of Astron., North. Polytech. Univ., Xi'an 710072, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2001年 / 22卷 / 02期
关键词：
Advection upstream splitting - Attack angle - Back pressure - Baldwin Lomax Turbulent model - Flight mach number - Flying altitude - MacCormack time splitting - Mixed compression inlet - Outlet - Supersonic inlet - Vector splitting;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：118 / 121
相关论文
共 50 条
  • [1] Euler flow in a supersonic mixed-compression inlet
    Jain, MK
    Mittal, S
    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2006, 50 (12) : 1405 - 1423
  • [2] Axisymmetric and three-dimensional flow simulation of a mixed compression supersonic air inlet
    Abedi, M.
    Askari, R.
    Sepahi-Younsi, J.
    Soltani, M. R.
    PROPULSION AND POWER RESEARCH, 2020, 9 (01) : 51 - 61
  • [3] Numerical simulation and experimental investigation on binary mixed-compression supersonic inlet
    Dong, Jia-Feng
    Li, Jin-Xian
    Cui, Jin-Ping
    Cao, Jun-Wei
    Wang, Hu-Gan
    Guti Huojian Jishu/Journal of Solid Rocket Technology, 2008, 31 (02): : 129 - 132
  • [4] Code for designing 2-D mixed-compression inlet of Solid Propellant Ramrocket
    Bao, Futing
    Li, Jinxian
    Zhao, Fei
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2002, 20 (04): : 590 - 593
  • [5] 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
  • [6] 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,
  • [7] 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
  • [8] Flow response hysteresis of throat regulation process of a two-dimensional mixed-compression supersonic inlet
    Yi JIN
    Shu SUN
    Huijun TAN
    Yue ZHANG
    Hexia HUANG
    Chinese Journal of Aeronautics , 2022, (03) : 112 - 127
  • [9] Flow response hysteresis of throat regulation process of a two-dimensional mixed-compression supersonic inlet
    Yi JIN
    Shu SUN
    Huijun TAN
    Yue ZHANG
    Hexia HUANG
    Chinese Journal of Aeronautics, 2022, 35 (03) : 112 - 127
  • [10] On the Possible Formation of a Vortex Flow in a Supersonic Inlet with Three-Dimensional Compression
    Lokotko, A. V.
    Kharitonov, A. M.
    FLUID DYNAMICS, 2006, 41 (04) : 649 - 660
12345