Thermal Effect on the Performance of an Alternating-Current Dielectric-Barrier-Discharge Plasma Actuator
Author:
Affiliation:
1. Nanyang Technological University, Singapore 639798, Republic of Singapore
2. The Hong Kong Polytechnic University, Hung Hom, Hong Kong, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference51 articles.
1. Flow Control on a NACA 4418 Using Dielectric-Barrier-Discharge Vortex Generators
2. Closed-Loop Dynamic Stall Control Using a Plasma Actuator
3. Flow Control on a Bluff Body Using Dielectric Barrier Discharge Plasma Actuators
4. Novel Sawtooth Dielectric Barrier Discharge Plasma Actuator for Flow Separation Control
5. Mechanism of Vorticity Generation in Plasma Streamwise Vortex Generators
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