Flow-Control Characteristics with Nanosecond-Pulse Plasma Actuator for Different Airfoil Shapes
Author:
Affiliation:
1. The University of Tokyo, Kashiwa 227-8568, Japan
2. Tohoku University, Sendai 980-8579, Japan
Funder
JSPS
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060486
Reference35 articles.
1. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
2. Development and characterization of plasma actuators for high-speed jet control
3. Flow Separation Control by Plasma Actuator with Nanosecond Pulsed-Periodic Discharge
4. Airflow control by non-thermal plasma actuators
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2. Flow Control around NACA0015 Airfoil Using a Dielectric Barrier Discharge Plasma Actuator over a Wide Range of the Reynolds Number;Actuators;2023-01-16
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