Aerodynamic Modification of NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap
AIAA Journal ; 47 , 10 ; 2467-2474
2009-10-01
Article (Journal)
Electronic Resource
English
Aerodynamic Modification of a NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap
Online Contents | 2009
|AIAA-2001-2483 Analysis of Gurney Flap Effects On A NACA 0012 Airfoil/Wing Section
British Library Conference Proceedings | 2001
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