Compressible dynamic stall control: Comparison of two approaches

Journal of Aircraft

Volumn 38, Issue 3, 2001, Pages 448-453

  Chandrasekhara, M S ^a   Wilder, M C ^a   Carr, L W ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FLOW CONTROL; HELICOPTER ROTORS; NUMERICAL METHODS; REYNOLDS NUMBER; UNSTEADY FLOW; VORTEX FLOW;

COMPRESSIBLE DYNAMIC STALL CONTROL; MACH NUMBER; SHAPE ADAPTING AIRFOIL; SLATTED AIRFOIL; UNSTEADY FLOW SEPARATION;

AIRFOILS;

EID: 0035334805     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2812     Document Type: Article

References (15)

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6. Controlled leading-edge suction for the management of unsteady separation over pitching airfoils
7. Oscillatory blowing: A tool to delay boundary layer separation
8. Separation control by periodic addition of momentum with particular emphasis on dynamic stall
9. Dynamic stall control by oscillatory forcing
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13. Dynamic stall control by variable airfoil camber
14. Aerodynamic characteristics of a rotorcraft airfoil designed for the tip region of a main rotor blade
15. The effect of compressibility on suppression of dynamic stall using a slotted airfoil