The effect of MHD interactions on the input shock waves in a supersonic diffuser

被引:7
作者
Bobashev, SV [1 ]
Vasil'eva, RV
D'yakonova, EA
Erofeev, AV
Lapushkina, TA
Maslennikov, VG
Ponyaev, SA
Sakharov, VA
van Wie, D
机构
[1] Russian Acad Sci, AF Ioffe Physicotech Inst, St Petersburg 194021, Russia
[2] Johns Hopkins Univ, Laurel, MD USA
基金
俄罗斯基础研究基金会;
关键词
Shock Wave; Mach Number; External Magnetic Field; Photography; Shock Tube;
D O I
10.1134/1.1345171
中图分类号
O59 [应用物理学];
学科分类号
摘要
The interaction with an external magnetic field modifies the variation of the shock wave configuration in a pure inert gas plasma at the entrance of a supersonic diffuser. The phenomenon was studied using an experimental setup based on a shock tube with a flat nozzle and the model supersonic diffuser. The experiments were conducted in krypton, for the shock wave Mach number in the shock tube M = 7.8 and the Mach number at the nozzle exit M = 4.2. The gasodynamic discontinuities and their structural variations induced by the magnetic induction changes were by visualized by the schlieren method and by photography of the intrinsic emission accompanying the process. Three regions of the MHD interaction affecting the shock wave configuration in the gas flow were revealed. (C) 2001 MAIK "Nauka/Interperiodica".
引用
收藏
页码:71 / 73
页数:3
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