Fabrication, surface integration and testing of miniaturized dielectric barrier discharge plasma actuators for active flow control applications-Reference-Cited by-同舟云学术

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Fabrication, surface integration and testing of miniaturized dielectric barrier discharge plasma actuators for active flow control applications

Published:2019-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aviation 2019 Forum
language:
Short-container-title:

Author:

Lindner Matthias G.¹,Berndt Dominik J.¹,Ehrlich Ingo¹,Jungbauer Bastian¹,Schreiner Rupert¹,Pipa Andrei²,Hink Rüdiger²,Foest Rüdiger²,Brandenburg Ronny²,Max Alexander³,Caspari Ralf³

Affiliation:

1. OTH Regensburg

2. INP Greifswald

3. Airbus

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Airflow control by non-thermal plasma actuators

2. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma

3. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators

4. Velocity-information-based force-term estimation of dielectric-barrier discharge plasma actuators

5. Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects

Cited by 2 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. Influence of dielectric thickness and electrode structure on the ion wind generation by micro fabricated plasma actuators;Journal of Physics D: Applied Physics;2020-07-17

2. Aircraft Icing Mitigation by DBD-based Micro Plasma Actuators;AIAA AVIATION 2020 FORUM;2020-06-08

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