Dynamic stall control for advanced rotorcraft application

AIAA Journal

Volumn 33, Issue 2, 1995, Pages 289-295

  Yu, Yung H ^a,c   Lee, Soogab ^a   McAlister, Kennth W ^a,c   Tung, Chee ^a,c   Wang, Clin M ^b  

^a US Army AMRDEC Development   (United States)

^b GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLADES; STALL;

AERODYNAMICS; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; CONTROL SYSTEMS; DRAG; FLOW VISUALIZATION; LIFT; MANEUVERABILITY; PERFORMANCE; TURBOMACHINE BLADES;

ACOUSTIC DETECTION; ACOUSTIC RADIATION; DYNAMIC STALL CONTROL; PITCHING MOMENT; ROTOR BLADES; ROTORCRAFT;

HELICOPTER ROTORS;

EID: 0029105982     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.12496     Document Type: Article

References (12)

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4. McAlister, K. W., and Tung, C., “Suppression of Dynamic Stall with a Leading-Edge Slat on a VR-7 Airfoil,” NASA-TP 3357, March 1993.
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8. Walker, G. J., Subroto, P. H., and Platzer, M. F., “Transition Modeling Effects on Viscous/Inviscid Interaction Analysis of Low Reynolds Number Airfoil Flows Involving Laminar Separation Bubbles,” American Society of Mechanical Engineers Gas Turbine Congress, ASME 88-GT-32, 1988.
9. Ekaterinaris, J. A., and Menter, F. R., “Computation of Separated and Unsteady Flows with One- and Two-Equation Turbulence Models,” AIAA Paper 94-0190, Jan. 1994.
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11. Lee, S., McAlister, K. W., and Tung, C., “Characteristics of a Deformable Leading-Edge for High Performance Helicopter Rotor,” AIAA Paper 93-3526, Aug. 1993.
12. Shrewsbury, G. D., “Evaluation of Research Circulation Control Airfoil Using Navier-Stokes Methods,” NASA-CP 2432, 1986.