Flight Control Using Wing-Tip Plasma Actuation
Author:
Affiliation:
1. École Polytechnique de Montréal, Montréal, Québec H3T 1J4, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44003
Reference35 articles.
1. Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology
2. A PIV Study of a Plasma Discharge Flow-Control Actuator on a Flat Plate in an Aggressive Pressure Induced Separation
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