Feedback Control of Flow Separation over Airfoil with Deep Reinforcement Learning in Numerical Simulation
Author:
Affiliation:
1. Tokyo Noko Daigaku Kogakubu Daigakuin Kogaku Kenkyuin
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1365
Reference17 articles.
1. Steady and Unsteady Plasma Wall Jets for Separation and Circulation Control
2. Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control
3. Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103–106
4. Mechanism of flow separation control with DBD plasma actuator obtained by Ape X Deep Q Network Control
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