Reflection of an Oblique Shock Wave in a Reacting Gas with a Finite Relaxation–Zone Length

被引：9
|
作者：
A. E. Medvedev
机构：
[1] Russian Academy of Sciences,Institute of Theoretical and Applied Mechanics, Siberian Division
来源：
Journal of Applied Mechanics and Technical Physics | 2001年 / 42卷 / 2期
关键词：
Reflection; Mathematical Modeling; Shock Wave; Mechanical Engineer; Heat Release;
D O I：
10.1023/A:1018811516116
中图分类号：
学科分类号：
摘要：
Reflection of an oblique shock wave in a reacting gas with a finite length of the chemical–reaction zone is studied. Shock polars for an arbitrary heat release behind the oblique shock wave are constructed. Transition criteria from regular to Mach reflection and back are obtained. It is shown that transition criteria are significantly changed if the reaction–zone length is taken into account.
引用
收藏
页码：211 / 218
页数：7
相关论文
共 4 条
  • [1] Underwater oblique shock wave reflection from submerged hydraulic structures
    Ghoshal, R.
    Mitra, N.
    OCEAN ENGINEERING, 2020, 209 (209)
  • [2] Experimental and numerical study of the reflection of an oblique shock wave in a stationary hypersonic flow.
    Chpoun, A
    Passerel, D
    Lengrand, JC
    Li, H
    BenDor, G
    RECHERCHE AEROSPATIALE, 1996, (02): : 95 - 105
  • [3] EFFECT OF RELAXATION PROCESSES ON THE SHOCK WAVE FOCUSING IN A GAS SUSPENSION CLOUD
    Sadin, D., V
    Belyaev, B., V
    Davidchuk, V. A.
    VESTNIK TOMSKOGO GOSUDARSTVENNOGO UNIVERSITETA-MATEMATIKA I MEKHANIKA-TOMSK STATE UNIVERSITY JOURNAL OF MATHEMATICS AND MECHANICS, 2020, (66): : 121 - 131
  • [4] Influence of the adiabatic index on switching between different types of shock wave reflection in a steady supersonic gas flow
    L. G. Gvozdeva
    S. A. Gavrenkov
    Technical Physics, 2013, 58 : 1238 - 1241
1