Deceleration of Supersonic Plasma Flow by an Applied Magnetic Field
| Autor: | Yurii Golovachov, David Van Wie, S. V. Bobashev |
|---|---|
| Rok vydání: | 2003 |
| Předmět: |
Physics
Mechanical Engineering Aerospace Engineering Plasma Mechanics Electromagnetic induction Magnetic field Physics::Fluid Dynamics Flow control (fluid) symbols.namesake Fuel Technology Classical mechanics Mach number Space and Planetary Science symbols Supersonic speed Magnetic pressure Choked flow |
| Zdroj: | Journal of Propulsion and Power. 19:538-546 |
| ISSN: | 1533-3876 0748-4658 |
| DOI: | 10.2514/2.6164 |
| Popis: | The problem of gas flow control by a magnetic field is considered as applied to flows in the intakes of supersonic aircraft. The method to be discussed for control of the intake operation consists of a preliminary ionization of incoming gas and subsequent control of the ionized flow by an applied magnetic field. To estimate the prospects of such a mode for flow control and the effects of the magnetogas dynamic interaction, a numerical investigation was conducted. The results demonstrate the possibility of controlling the flow structure at reasonable plasma and magnetic field parameters. The effects of magneto-gas dynamic interaction on supersonic flow deceleration are investigated. |
| Databáze: | OpenAIRE |
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