Aerodynamic Performance Modification at Low Angles of Attack by Trailing Edge Vortices
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[1] A. Glezer,et al. The formation and evolution of synthetic jets , 1998 .
[2] I. Wygnanski,et al. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation , 1993 .
[3] A. W. Bloy,et al. Enhanced Aerofoil Performance Using Small Trailing-Edge Flaps , 1997 .
[4] M. Amitay,et al. Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators , 2001 .
[5] David W. Hurst,et al. Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing , 2000 .
[6] Kai Richter,et al. Experimental investigation of trailing-edge devices at transonic speeds , 2002 .
[7] F. Hsiao,et al. Control of wall-separated flow by internal acoustic excitation , 1990 .
[8] Roy Y. Myose,et al. Gurney Flap Experiments on Airfoils, Wings, and Reflection Plane Model , 1998 .
[9] R. Liebeck. Design of Subsonic Airfoils for High Lift , 1976 .