Aerodynamic Modification of NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap
AIAA Journal ; 47 , 10 ; 2467-2474
01.10.2009
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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
|