Effect of Mach number on the efficiency of microwave energy deposition in supersonic flow

被引:14
|
作者
Lashkov, V. A. [1 ]
Karpenko, A. G. [1 ]
Khoronzhuk, R. S. [2 ]
Mashek, I. Ch. [2 ]
机构
[1] St Petersburg State Univ, Dept Math & Mech, St Petersburg 199034, Russia
[2] St Petersburg State Univ, Dept Phys, St Petersburg 199034, Russia
基金
俄罗斯基础研究基金会;
关键词
RELEASE;
D O I
10.1063/1.4949524
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The article is devoted to experimental and numerical studies of the efficiency of microwave energy deposition into a supersonic flow around the blunt cylinder at different Mach numbers. Identical conditions for energy deposition have been kept in the experiments, thus allowing to evaluate the pure effect of varying Mach number on the pressure drop. Euler equations are solved numerically to model the corresponding unsteady flow compressed gas. The results of numerical simulations are compared to the data obtained from the physical experiments. It is shown that the momentum, which the body receives during interaction of the gas domain modified by microwave discharge with a shock layer before the body, increases almost linearly with rising of Mach number and the efficiency of energy deposition also rises. Published by AIP Publishing.
引用
收藏
页数:6
相关论文
共 50 条
  • [21] Visualization of supersonic unequal Mach number twin jet
    Vinoth, BR
    Rathakrishnan, E
    JOURNAL OF VISUALIZATION, 2005, 8 (04) : 290 - 290
  • [22] Mach Number and Heating Effects on Turbulent Supersonic Jets
    Georgiadis, Nicholas J.
    Wernet, Mark P.
    Locke, Randy J.
    Eck, Dennis. G.
    AIAA JOURNAL, 2024, 62 (01) : 31 - 51
  • [23] Approach to Determine the Most Efficient Supersonic Mach Number
    Shi, Aiming
    Chen, Jinduo
    Dowell, Earl H.
    Wen, Hao
    AIAA JOURNAL, 2020, 58 (03) : 1402 - 1406
  • [24] Effects of Mach number on supersonic wraparound fin aerodynamics
    McIntyre, TC
    Bowersox, RDW
    Goss, LP
    JOURNAL OF SPACECRAFT AND ROCKETS, 1998, 35 (06) : 742 - 748
  • [25] Effects of Mach Number on the Performance of a Diverterless Supersonic Inlet
    Askari, R.
    Solani, M. R.
    JOURNAL OF AIRCRAFT, 2019, 56 (04): : 1697 - 1707
  • [26] Visualization of supersonic unequal mach number twin jet
    B. R. Vinoth
    E. Rathakrishnan
    Journal of Visualization, 2005, 8 : 290 - 290
  • [27] Pulsed Laser Energy Deposition in Supersonic Flow Over a Cylinder
    Chauhan, Anurag
    Pattankar, Rohan
    Ghosh, Shankar
    AIAA SCITECH 2022 FORUM, 2022,
  • [28] INFLUENCE OF MACH NUMBER AND SHAPE OF FRONT PART ON LENGTH OF SEPARATION REGION IN SUPERSONIC-FLOW
    VINOGRADOV, YA
    ZUBKOV, AI
    LYAGUSHIN, BE
    PANOV, YA
    YAKUSHEV, SA
    VESTNIK MOSKOVSKOGO UNIVERSITETA SERIYA 1 MATEMATIKA MEKHANIKA, 1990, (04): : 93 - 95
  • [29] Exact relation for determining the pressure distribution on a sphere at an arbitrary mach number in a supersonic incoming flow
    Kotenev V.P.
    Mathematical Models and Computer Simulations, 2015, 7 (2) : 128 - 133
  • [30] Effect of Mach number on transonic flow past a circular cylinder
    XU ChangYue CHEN LiWei LU XiYun Department of Modern Mechanics University of Science and Technology of China Hefei China
    Chinese Science Bulletin, 2009, 54 (11) : 1886 - 1893