Total Drag and Lift Measurements in a Mach 5 Flow Affected by a Plasma Discharge and a Magnetic Field-Reference-Cited by-同舟云学术

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Total Drag and Lift Measurements in a Mach 5 Flow Affected by a Plasma Discharge and a Magnetic Field

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Menart James¹,Shang Joseph¹,Atzbach C.¹,Magoteaux S.¹,Slagel M.¹,Bilheimer B.¹

Affiliation:

1. Wright State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-947

Reference32 articles.

1. The Effect of Plasma Induced Separation

2. Active Control of High Speed Jets Using Localized Arc Filament Plasma Actuators

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1. Drag Reduction Technology of Jet - A Review;International Journal of Engineering Research in Africa;2015-07

2. Experimental investigations on the magneto-hydro-dynamic interaction around a blunt body in a hypersonic unseeded air flow;Journal of Applied Physics;2012-11

3. MHD Interaction around a Blunt Body in a Hypersonic Unseeded Air Flow: Experimental Results and Numerical Rebuilding;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

4. Experimental Investigations on the MHD Interaction Around a Blunt Body in a Hypersonic Unseeded Air Flows;43rd AIAA Plasmadynamics and Lasers Conference;2012-06-25

5. Effect of a Counterflow Plasma Jet on Aerodynamics Characteristic of a Blunted Cone;28th International Symposium on Shock Waves;2012

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