Thrust Vectoring Flow Control Using Plasma Synthetic Jet Actuators
Author:
Affiliation:
1. Oklahoma State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1368
Reference21 articles.
1. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma
2. Application of weakly-ionized plasmas as wing flow-control devices
3. Demonstration of Separation Delay with Glow Discharge Plasma Actuators
4. Separation Control Using Plasma Actuators: Dynamic Stall Control on an Oscillating Airfoil
5. Plasma-Based Actuators for Cylinder Wake Vortex Control
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