Plasma Effect on Shocks Configuration in Compression Ramp-Reference-Cited by-同舟云学术

Plasma Effect on Shocks Configuration in Compression Ramp

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Leonov Sergey¹,Firsov Alexander¹,Yarantsev Dmitry¹,Falempin Francois²,Goldfeld Marat³

Affiliation:

1. Russian Academy of Sciences

2. MBDA

3. Khristianovich Institute of Theoretical and Applied Mechanics

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2362

Reference18 articles.

1. Near-Surface Electrical Discharge in Supersonic Airflow: Properties and Flow Control

2. S. Macheret, R. Miles, M. Schneider, "Comparative analysis of MHD and plasma methods of scramjet inlet control", AIAA-2003-0170,41thAIAAAerospaceMeetingandExhibit,6-10January,Reno,NV,2003.

3. J.S. Shang, S.T. Surzhikov, R. Kimmel et al. "Mechanisms of Plasma Actuators For Hypersonic Flow Control //Progress inAerospace Sciences", 2005,Vol.41, pp.642-668.

4. Airflow control by non-thermal plasma actuators

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