Control of Separated Flow on a NACA 0015 Airfoil using Three-Dimensional Plasma Actuator (AIAA 2014-2665)
Conference; 7th, Flow control; 7th AIAA flow control conference 2014; Atlanta, Georgia, USA, 16-20 June 2014 : held at the AIAA aviation forum 2014 ; 2014 ; Atlanta, GA
2014-01-01
10 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
AIAA , Flow control , Aviation , Aeronautics
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Reduced Order Modeling of Flow over a NACA 0015 Airfoil for Control Application (AIAA 2014-2516)
British Library Conference Proceedings | 2014
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