Interaction of Microwave-Generated Plasma with Hemisphere-Cone-Cylinder

Author:

Knight Doyle1,Kolesnichenko Yuri2,Brovkin Vadim2,Lashkov Valery3,Mashek Igor3

Affiliation:

1. Rutgers University

2. Russian Academy of Sciences

3. Saint-Petersburg State University

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. Scramjet Inlet Control by Off-Body Energy Addition: a Virtual Cowl

2. 2Girgis, I., Schneider, M., Macheret, S., Brown, G., and Miles, R. “Creation of Steering Moments in Supersonic Flow by Off-Axis Plasma Heat Addition,” Tech. Rep. 2002-0129, American Institute of Aeronautics and Astronautics, January 2002.

3. Basics in Beamed MW Energy Deposition for Flow/Flight Control

4. Gas-Dynamic Effects Around the Body Under Energy Deposition in Supersonic Flow

5. Gas-Dynamic Peculiarities of Microwave Discharge Interaction with Shock Wave Near the Body

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