Effect of dielectric barrier discharge plasma actuators on non-equilibrium hypersonic flows-Reference-Cited by-同舟云学术

Effect of dielectric barrier discharge plasma actuators on non-equilibrium hypersonic flows

Published:2014-10-28 Issue:16 Volume:116 Page:164904
ISSN:0021-8979
Container-title:Journal of Applied Physics
language:en
Short-container-title:Journal of Applied Physics

Author:

Bhatia Ankush¹,Roy Subrata¹,Gosse Ryan²

Affiliation:

1. Applied Physics Research Group, Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville 32611, USA

2. Computational Sciences Center of Excellence, Air Force Research Laboratory, AFRL/RQHV, Bldg 146B, 2210 Eighth St., WPAFB, Ohio 45433-7512, USA

Funder

UES, Inc. (flow through of a AFRL grant)

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/1.4898862

Reference51 articles.

1. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma

2. F. Soetomo , “ The influence of high voltage discharge on flat plate drag at low Reynolds number air flow,” MS thesis (Iowa State University, 1992).

3. Influence of a DC corona discharge on the airflow along an inclined flat plate

4. Control of low velocity airflow along a flat plate with a DC electrical discharge

5. Effect of a DC surface-corona discharge on a flat plate boundary layer for air flow velocity up to 25m/s

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