Deceleration of Supersonic Plasma Flow by an Applied Magnetic Field
Author:
Affiliation:
1. Ioffe Physico-Technical Institute RAS
2. Johns Hopkins University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2247
Reference16 articles.
1. Gurijanov E. P. and Harsha P. T. "AJAX: New Directions in Hypersonic Technology," PaperAIAA-96-4609.
2. Use of MHD systems in hypersonic aircraft
3. Magnetic-field control of gas flow in a supersonic intake
4. Vatazhin A. B., Kopchenov V. I., and Gouskov O. V. "Some Estimation of Possibility to Use the MHD Control for Hypersonic Flow Deceleration," Paper AIAA-99-4972.
5. Golovachov Yu. P., Sushchikh S. Yu, and Van Wie D. M. "Numerical Simulation of MGD Flows in Supersonic Inlets," Paper AIAA-2000-2666.
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1. Parameter Research of an MHD Controlled Inlet;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02
2. Control Volume Approach to Quasi-1D Flow Control within Electromagnetic Fields;39th Plasmadynamics and Lasers Conference;2008-06-15
3. Effect of Magnetohydrodynamics Interaction in Various Parts of Diffuser on Inlet Shocks: Experiment;Journal of Propulsion and Power;2005-09
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