Effect of Burst Frequency and Reynolds Number on Flow Control Authority of DBD Plasma Actuator on NACA0012 Airfoil (AIAA 2014-1245)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
21 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 2014
|Low-Reynolds-number effect on the aerodynamic characteristics of a pitching NACA0012 airfoil
Online Contents | 2014
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