Investigation of magnetohydrodymamic interaction in a supersonic air flow at M=8

被引：2
|
作者：
Korotaeva, T. A. [1 ]
Fomichev, V. P. [1 ]
Shashkin, A. P. [1 ]
Yadrenkin, M. A. [1 ]
机构：
[1] Russian Acad Sci, Siberian Branch, Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia
来源：
TECHNICAL PHYSICS | 2011年 / 56卷 / 03期
关键词：
Shock Wave; Electron Beam; Slope Angle; Shock Tube; Hypersonic Flow;
D O I：
10.1134/S1063784211030108
中图分类号：
O59 [应用物理学];
学科分类号：
摘要：
The influence of magnetohydrodynamic interaction localized before a model on the position of a shock wave attached to a wedge is experimentally and numerically investigated. The investigation is carried out in an air flow with a Mach number of 8. It is shown that, for a hydromagnetic interaction parameter on the order of 0.1, the slope angle of the shock wave can be increased by 10A degrees. Experiments are conducted for the case when the flow is ionized by an electron beam or by a pulsed electric discharge. Good agreement between experimental and numerical results is obtained for both ways of ionization if the Joule heating of the gas is insignificant. The conclusion is drawn that the way of providing a nonequilibrium conductivity of the flow has a minor effect on the position of the oblique shock wave near the wedge with the hydromagnetic interaction parameter being the same.
引用
收藏
页码：327 / 334
页数：8
相关论文
共 50 条
  • [1] Investigation of magnetohydrodymamic interaction in a supersonic air flow at M = 8
    T. A. Korotaeva
    V. P. Fomichev
    A. P. Shashkin
    M. A. Yadrenkin
    Technical Physics, 2011, 56
  • [2] Studying the interaction of supersonic air flow with transverse discharge
    S. V. Bobashev
    V. P. Belik
    N. A. Monakhov
    M. V. Petrenko
    P. A. Popov
    V. A. Sakharov
    Technical Physics Letters, 2015, 41 : 1107 - 1109
  • [3] Studying the interaction of supersonic air flow with transverse discharge
    Bobashev, S. V.
    Belik, V. P.
    Monakhov, N. A.
    Petrenko, M. V.
    Popov, P. A.
    Sakharov, V. A.
    TECHNICAL PHYSICS LETTERS, 2015, 41 (11) : 1107 - 1109
  • [4] Numerical investigation of air flow in a supersonic wind tunnel
    Drozdov, S. M.
    Rtishcheva, A. S.
    INTERNATIONAL CONFERENCE PROBLEMS OF THERMAL PHYSICS AND POWER ENGINEERING (PTPPE-2017), 2017, 891
  • [5] Experimental Investigation of Flow Interaction Dynamics in Supersonic Retropropulsion
    Mejia, N. A.
    Schmidt, B. E.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2022, 59 (05) : 1753 - 1762
  • [6] Investigation of Supersonic Jet Interaction With Hypersonic Cross Flow
    Desikan, S. L. N.
    Saravanan, R.
    Subramanian, S.
    Sivararamakrishnan, A. E.
    Pandian, S.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2015, 137 (10):
  • [7] Experimental investigation of side jet interaction with a supersonic cross flow
    Stahl, B.
    Esch, H.
    Guelhan, A.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2008, 12 (04) : 269 - 275
  • [8] PIV investigation of supersonic base-flow-plume interaction
    van Oudheusden, Bas W.
    Scarano, Fulvio
    PARTICLE IMAGE VELOCIMETRY: NEW DEVELOPMENTS AND RECENT APPLICATIONS, 2008, 112 : 465 - 474
  • [9] Numerical Investigation of Multiple Shock/Turbulent Flow Interaction in a Supersonic Channel
    Sun, Peizhao
    Yang, Jiming
    Lu, Xiyun
    ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2018, 10 (02) : 390 - 408
  • [10] The interaction between plasma jet of a capillary discharge and transverse supersonic air flow
    Ershov, A. P.
    Kolesnikov, E. B.
    Timofeev, I. B.
    Chernikov, V. A.
    Chuvashev, S. N.
    Shibkov, V. M.
    HIGH TEMPERATURE, 2007, 45 (05) : 580 - 587
12345