Shock impinge on supersonic cross flow injection

被引：0
|
作者：
Pan, Yu [1 ]
Wang, Zhen-Guo [1 ]
机构：
[1] College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
来源：
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology | 2007年 / 29卷 / 06期
关键词：
7;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：6 / 9
相关论文
共 50 条
  • [31] Unsteady transverse injection of kerosene into a supersonic flow
    Xu, SL
    Archer, RD
    Milton, BE
    Yue, PT
    SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2000, 43 (02): : 206 - 214
  • [32] Numerical investigation of a supersonic flow with jet injection
    Naimanova, A. Zh.
    Advances in High Performance Computing and Computational Sciences, 2006, 93 : 139 - 150
  • [33] Hydrogen Injection Scheme Influence on Flow Structure in Supersonic Combustor of Constant Cross-Section
    Starov, A. V.
    Goldfeld, M. A.
    PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017), 2017, 1893
  • [34] Transverse and parallel injection of hydrogen with supersonic combustion in a shock tunnel
    Wendt, MN
    Stalker, RJ
    SHOCK WAVES, 1996, 6 (01) : 53 - 59
  • [35] Transforming the shock pattern of supersonic jets using fluidic injection
    Semlitsch, Bernhard
    Cuppoletti, Daniel R.
    Gutmark, Ephraim J.
    Mihăescu, Mihai
    AIAA Journal, 2019, 57 (05): : 1851 - 1861
  • [36] Transforming the Shock Pattern of Supersonic Jets Using Fluidic Injection
    Semlitsch, Bernhard
    Cuppoletti, Daniel R.
    Gutmark, Ephraim J.
    Mihaescu, Mihai
    AIAA JOURNAL, 2019, 57 (05) : 1851 - 1861
  • [37] Shock tunnel measurement of the interaction amplification factor for a hot gas side jet in a supersonic cross flow
    Havermann, M
    Ende, H
    Seiler, F
    Schwenzer, M
    Shock Waves, Vols 1 and 2, Proceedings, 2005, : 113 - 118
  • [38] One Case of Shock-free Deceleration of a Supersonic Flow in a Constant Cross Section Area Channel
    Khazov D.E.
    Supercomputing Frontiers and Innovations, 2022, 9 (04) : 18 - 27
  • [39] RESPONSE OF A PLATE IN SUPERSONIC FLOW TO A SHOCK LOAD.
    Dzygadlo, Z.
    Olejnik, A.
    Polish Academy of Sciences, Institute of Fundamental Technical Research, Proceedings of Vibration Problems, 1973, 14 (02): : 165 - 180
  • [40] Stability of transonic shock for supersonic flow past a wedge
    Peng, Weimin
    Hu, Dian
    MATHEMATICAL METHODS IN THE APPLIED SCIENCES, 2016, 39 (07) : 1891 - 1907
12345