Pulsed Discharge Actuators for Rectangular Wing Separation Control-Reference-Cited by-同舟云学术

Pulsed Discharge Actuators for Rectangular Wing Separation Control

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Sidorenko Andrey¹,Zanin Boris¹,Postnikov Boris¹,Budovsky Alexey¹,Starikovskii Andrei²,Roupassov Dmitry²,Zavialov Ivan²,Malmuth Norman³,Smereczniak Philip⁴,Silkey Joseph⁴

Affiliation:

1. Institute of Theoretical and Applied Mechanics

2. Moscow Institute of Physics and Technology

3. Teledyne Scientific Company

4. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-941

Reference9 articles.

1. Post-stall flow control on an airfoil by local unsteady forcing

2. Overview of Plasma Flow Control: Concepts, Optimization, and Applications

3. A. A. Maslov, B. Yu. Zanin,A.A. Sidorenko, B. VPostnikov, V. P. Fomichev,A. D.Budovsky andN.Malmuth, "Two-Channel Spark Discharge for Flow Control on a Body of Revolution," AIAA Paper No. 2005-040, Reno NV, 10-13January 2005

4. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma

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