Parametric and Numerical Investigations of Scramjet with MHD Bypass

Author:

Sheikin Evgeniy1

Affiliation:

1. Hypersonic Systems Research Institute

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Use of MHD systems in hypersonic aircraft

2. 3SheikinE.G.,andKuranovA.L."ScramjetwithMHDBypassunder"AJAX"concept,"AIAAPaper2004-1192.

3. 4AbramovichG.N."AppliedGasDynamics,"Nauka,Moscow,1976(inRussian).

4. KuranovA.L.,andSheikinE.G."MHDControlbyExternalandInternalFlowsinScramjetunder"Ajax"Concept,"AIAA Paper 2003-0173.

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1. Three-dimensional numerical analyses on magnetohydrodynamic accelerator;Energy Conversion and Management;2007-08

2. Variable Properties Argon Plasma Flow in a Faraday Generator;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

3. Scramjet with MHD Controlled Inlet;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

4. MHD Control in Hypersonic Aircraft;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

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