Role of actuation frequency in controlled flow reattachment over a stalled airfoil

AIAA Journal

Volumn 40, Issue 2, 2002, Pages 209-216

  Amitay, Michael ^a   Glezer, Ari ^a  

^a GEORGIA TECH RESEARCH INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRFOILS; FLUIDIC DEVICES; UNSTEADY FLOW; VORTEX FLOW; VORTEX SHEDDING; WIND TUNNELS;

FLOW REATTACHMENT; STALLED AIRFOIL; SURFACE MOUNTED FLUIDIC ACTUATORS;

AERODYNAMICS;

EID: 0036472043     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1662     Document Type: Article

References (17)

1. Design and engineering features of flap blowing installations
2. Delay of airfoil stall by periodic excitation
3. Separation control on an airfoil under post-stall conditions by mechanical excitation
4. Moving surface boundary layer control as applied to slender and bluff bodies
5. Control of flow separation by sound
6. Forcing level effects of internal acoustic excitation on the improvement of airfoil performance
7. Modification of lifting body aerodynamics using synthetic jet actuators
8. Aerodynamic flow control using synthetic jet technology
9. Flow reattachment dynamics over a thick airfoil controlled by synthetic jet actuators
10. Separation control on a post-stall airfoil using acoustically generated perturbations
11. Modification of the aerodynamics characteristics of an unconventional airfoil using synthetic jet actuators
12. The formation and evolution of synthetic jets
13. Active flow control applied to an airfoil
14. Post-stall control on an airfoil by local unsteady forcing
15. Oscillatory control of separation at high Reynolds numbers