Advancement of scramjet MHD concept-Reference-Cited by-同舟云学术

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Advancement of scramjet MHD concept

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Burakhanov B.¹,Likhachev A.¹,Medin S.¹,Novikov V.¹,Okunev V.¹,Rickman V.¹

Affiliation:

1. Russian Academy of Sciences, Associated Inst. of High Temperatures, Moscow, Russia

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-614

Reference13 articles.

1. Mixing-Controlled Supersonic Combustion

2. Gurjanov E.P. and Harsha P.T. AJAX: New directions in hypersonic technology, AIAA Pap. No 96-4609.

3. Brichkin D.I., Kuranov A.L., Sheikin E.G. MHD technology for scramjet control. AIAA Pap. No 98-1642.

4. Bruno C'. and Czy.szP.A. An electro-magneticchemical hypersonic propulsion system. AIAA Pap. No 98-1582.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Flow Control of Hypersonic Separated Flows by Applied Magnetic Fields;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

2. Numerical Simulation of Magnetohydrodynamic Flows;Journal of Spacecraft and Rockets;2004-07

3. MHD Flow Control Concepts for Pulse Detonation Engines;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15

4. Numerical Simulation of MHD Flows with the Generalized Ohm's Law;41st Aerospace Sciences Meeting and Exhibit;2003-01-06

5. Large Eddy Simulation of Turbulent Magnetohydrodynamic Flows;41st Aerospace Sciences Meeting and Exhibit;2003-01-06

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