Flow Structure Modification Using Plasma Actuation for Enhanced UAV Flight Control
Author:
Affiliation:
1. Experimental Aerodynamics Branch; INTA; Madrid Spain
Publisher
John Wiley & Sons, Ltd
Reference51 articles.
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4. Corke , T.C. Jumper , E.J. Post , M.L. Orlov , D. McLaughlin , T.E. 2002 Applications of weakly-ionized plasmas as wing flow-control devices 40th AIAA Aerospace Sciences Meeting and Exhibit
5. Post , M.L. Corke , T.C. 2004 Separation control using plasma actuators - dynamic stall control on an oscillating airfoils 2nd AIAA Flow Control Conference
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