Flow Separation Control over a Thin Post-Stall Airfoil: Effects of Excitation Frequency
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43235
Funder
Army Research Office
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057796
Reference44 articles.
1. Airflow control by non-thermal plasma actuators
2. Dielectric Barrier Discharge Plasma Actuators for Flow Control
3. Capabilities of the dielectric barrier discharge plasma actuator for multi-frequency excitations
4. Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control
5. Scaling Effects of an Aerodynamic Plasma Actuator
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