Magnetic-field control of gas flow in a supersonic intake

被引:4
作者
Golovachev, YP [1 ]
Il'in, SA [1 ]
Sushchikh, SY [1 ]
机构
[1] Russian Acad Sci, AF Ioffe Physicotech Inst, St Petersburg 196140, Russia
关键词
Magnetic Field; External Magnetic Field; Flow Structure; Supersonic Aircraft; Supersonic Intake;
D O I
10.1134/1.1261772
中图分类号
O59 [应用物理学];
学科分类号
摘要
A numerical simulation is used to assess the potential for controlling the how structure in the air intake of a supersonic aircraft by means of an external magnetic field. (C) 1997 American Institute of Physics. [S1063-7850(97)01808-9].
引用
收藏
页码:615 / 616
页数:2
相关论文
共 2 条
[1]  
Mitchner M, 1973, Partially Ionized Gases
[2]  
Rodionov A. V., 1987, Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, V27, P1853