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Numerical investigation of non-equilibrium MGD flows in supersonic intakes

  • Published:2001-06-11 Issue: Volume: Page:
  • ISSN:
  • Container-title:32nd AIAA Plasmadynamics and Lasers Conference
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Author:

Golovachov Yurii1,Kurakin Yurii1,Schmidt Alexander1,Van Wie David2

Affiliation:

1. Russian Academy of Sciences, Ioffe Physical Technical Inst., St. Petersburg, Russia

2. Johns Hopkins Univ., Laurel, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Magnetic-field control of gas flow in a supersonic intake

2. "MHD-technology for Scramjet Control", AIAA Paper 98-1642. [3]. Golovachov Yu.R, Sushchikh S.Yu., and Van

3. Wie D.M. "Numerical Simulation of MGD Flows in Supersonic Inlets", AIAA Paper 2000-2666. [4]. Bobashev S.V., et al. "Shock Tube Facility for

4. MGD Supersonic Flow Control", AIAA Paper 2000-2647. [5]. Mitchner M. and Kruger C.H. Jr. PartiallyIon

5. ized Gases. Wiley & Sons, 1973. [6]. Biberman L.M., Vorob'ev V.S., Yakubov I.T.

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