The Influence of Electrode Configuration and Dielectric Temperature on Plasma Actuator Performance

Author:

Erfani Rasool1,Hale Craig1,Kontis Konstantinos1

Affiliation:

1. University of Manchester

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. MEE-DBD Plasma Actuator Effect on Aerodynamics of a NACA0015 Aerofoil: Separation and 3D Wake;Advances in Effective Flow Separation Control for Aircraft Drag Reduction;2019-10-18

2. Numerical Analysis of Anti-Icing Property of NSDBD Plasma Actuator on Airfoil;9th AIAA Atmospheric and Space Environments Conference;2017-06-02

3. Experimental Study of Anti-icing and Deicing on a Cylinder by DBD plasma actuation;47th AIAA Plasmadynamics and Lasers Conference;2016-06-10

4. Multiple Encapsulated Electrode Plasma Actuator Effect on Aerofoil-Wake Interaction;44th AIAA Plasmadynamics and Lasers Conference;2013-06-22

5. Optimisation of multiple encapsulated electrode plasma actuator;Aerospace Science and Technology;2013-04

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