Stall control with local surface buzzing on a NACA 0012 airfoil

AIAA Journal

Volumn 39, Issue 7, 2001, Pages 1400-1402

  Park, Y W ^a   Lee, S G ^a   Lee, D H ^a   Hong, S ^a  

^a Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW VISUALIZATION; LIFT; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; SPECTRUM ANALYSIS; VELOCITY MEASUREMENT; VORTEX FLOW;

STALL CONTROL; VIBRATING RIBBON METHOD;

AIRFOILS;

EID: 0035398369     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1460     Document Type: Article

References (8)

1. Dynamic stall control for advanced rotorcraft application
2. High-incidence airfoil aerodynamics improvement by leading-edge oscillating flap
3. Delay of airfoil stall by periodic excitation
4. Oscillatory blowing: A tool to delay boundary-layer separation
5. Separation control on an airfoil by periodic forcing
6. Flow structures behind a vertically oscillating fence immersed in a flat-plate turbulent boundary layer
7. Use of piezoelectric actuators for airfoil separation control
8. Some factors affecting stall control with particular emphasis on dynamic stall