Modeling and Parametric Study of a Plasma Synthetic Jet for Flow Control
Author:
Affiliation:
1. Université de Toulouse, 31062 Toulouse, France
2. ONERA-DTIM, ONERA–The French Aerospace Lab, Toulouse 31055, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052521
Reference24 articles.
1. Plasmas for aerodynamic control
2. Sparkjet Actuators for Flow Control
3. Computational Assessment of the SparkJet Flow Control Actuator
4. The "Plasma Synthetic Jet" Actuator. Aero-thermodynamic Characterization and First Flow Control Applications.
5. Investigation of plasma-generated jets for supersonic flow control
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