Structure of the Current Layer and Modes of Magneto-Gasdynamic Interaction with Supersonic Gas Flow

被引：1
|
作者：
Vasil'ev, E. N. [1 ]
Nesterov, D. A. [1 ]
机构：
[1] Russian Acad Sci, Inst Computat Modeling, Siberian Branch, Krasnoyarsk, Russia
来源：
HIGH TEMPERATURE | 2019年 / 57卷 / 05期
基金：
俄罗斯基础研究基金会;
关键词：
NUMERICAL-SIMULATION; MAGNETOGASDYNAMIC INTERACTION; SPATIAL STRUCTURE; ELECTRIC-ARC;
D O I：
10.1134/S0018151X19050183
中图分类号：
O59 [应用物理学];
学科分类号：
摘要：
Numerical simulation of the interaction of the current layer in the magneto-gasdynamic channel with the induction of external magnetic fields of 1, 2, and 4 T and various load resistance values has been carried out. Features of the energy balance and differences in the temperature profiles in the current layers, which were both streamlined by a nonconducting gas flow and completely covered the channel cross section and interacted with the flow like a piston, are revealed. The dependences on the load resistance are obtained for the current, coefficients of current-layer permeability, and enthalpy conversion.
引用
收藏
页码：603 / 608
页数：6
相关论文
共 50 条
  • [21] INTERACTION OF SHOCK WAVES AND BOUNDARY LAYERS IN SUPERSONIC GAS FLOW
    WINCKLER, J
    PHYSICAL REVIEW, 1946, 69 (11-1): : 678 - 678
  • [22] Interaction of the transversal gas jet with supersonic flow in the dihedral angle
    Zubkov, A.I.
    Lyagushin, B.E.
    Panov, Yu.A.
    Tul'tsev, A.V.
    Izvestiya Akademii Nauk. Mekhanika Zhidkosti I Gaza, 1994, (06): : 161 - 165
  • [23] A nanosecond high-current discharge in a supersonic gas flow
    Znamenskaya, IA
    Koroteev, DA
    Popov, NA
    HIGH TEMPERATURE, 2005, 43 (06) : 817 - 824
  • [24] A Nanosecond High-Current Discharge in a Supersonic Gas Flow
    I. A. Znamenskaya
    D. A. Koroteev
    N. A. Popov
    High Temperature, 2005, 43 : 817 - 824
  • [25] Flow structure formed by interaction of a single microjet with a supersonic jet flow
    Zapryagaev, V. I.
    Kiselev, N. P.
    JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2009, 50 (03) : 447 - 453
  • [26] Flow structure formed by interaction of a single microjet with a supersonic jet flow
    V. I. Zapryagaev
    N. P. Kiselev
    Journal of Applied Mechanics and Technical Physics, 2009, 50 : 447 - 453
  • [27] Measurements of compressible turbulent flow structure in a supersonic mixing layer
    Bowersox, R.D.W.
    Schetz, J.A.
    AIAA Journal, 1995, 33 (11): : 2101 - 2106
  • [28] TURBULENT BOUNDARY-LAYER STRUCTURE IN SUPERSONIC-FLOW
    SMITS, AJ
    PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1991, 336 (1641): : 81 - 93
  • [29] DNS of Shock/Boundary Layer Interaction Flow in a Supersonic Compression Ramp
    Li, Xin-Liang
    Fu, De-Xun
    Ma, Yan-Wen
    Liang, Xian
    COMPUTATIONAL FLUID DYNAMICS 2010, 2011, : 729 - 737
  • [30] Interaction of an external supersonic flow with the subsonic layer near a wavy wall
    Smelova N.V.
    Fluid Dynamics, 1997, 32 (1) : 79 - 85
12345