Flow Reattachment and Vortex Re-formation on Oscillating Low-Aspect-Ratio Wings
Attenuation of Self-Excited Roll Oscillations of Low-Aspect-Ratio Wings by Using Acoustic Forcing
Lift-Enhancing Vortex Flows Generated by Plunging Rectangular Wings with Small Amplitude
Lift Enhancement of a Flat-Plate Airfoil by Steady Suction
Lift Enhancement by Means of Small-Amplitude Airfoil Oscillations at Low Reynolds Numbers