Shock reflexion and shock-wave interaction in field-aligned flows
Abstract
This paper considers the steady two-dimensional problem of regular reflexion and symmetric intersection of oblique magnetogasdynamic shock waves. It is assumed that the fluid medium is a non-viscous, non-heat-conducting, ideal gas of infinite electrical conductivity, and that the applied magnetic field is parallel to the velocity of the approaching stream. In view of the complexity of the shock relations, a graphical method is presented for determining the orientation and strength of the reflected shock wave in terms of the Laval number M*1 (flow speed divided by critical sound speed), the Alfvén number A1 (flow speed divided by Alfvén speed), and the shock angle 1 ahead of the incident shock. Moreover, the possible ranges of M*1, A1, and 1, for which regular reflexion may occur, are calculated and illustrated graphically for the case of a monatomic gas.
- Publication:
-
Journal of Plasma Physics
- Pub Date:
- August 1975
- DOI:
- Bibcode:
- 1975JPlPh..14...39N
- Keywords:
-
- Magnetohydrodynamic Waves;
- Oblique Shock Waves;
- Shock Wave Interaction;
- Supersonic Flow;
- Two Dimensional Flow;
- Wave Reflection;
- Flow Distribution;
- Ideal Gas;
- Laval Number;
- Lines Of Force;
- Magnetic Fields;
- Magnetic Induction;
- Magnetoacoustic Waves;
- Shock Fronts;
- Turbulent Flow;
- Vectors (Mathematics);
- Plasma Physics