Bang-Bang Control Applied in Airfoil Roll Control with Plasma Actuators
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Peking University, Beijing 100871, People’s Republic of China
2. Aerodynamics Research Institute, Aviation Industry Corporation of China, Harbin 150001, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031964
Reference14 articles.
1. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma
2. Airflow control by non-thermal plasma actuators
3. Active Control of a High Reynolds Number Mach 0.9 Axisymmetric Jet
4. Feasibility Study for Steering a Supersonic Projectile by a Plasma Actuator
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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