Airfoil dynamic stall at constant pitch rate and high Reynolds number
- 8 June 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Aerodynamic testing at low Reynolds numbersJournal of Aircraft, 1987
- Lift-curve characteristics for an airfoil pitching at constant ratePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Airfoil dynamic stall performance with large-amplitude motionsAIAA Journal, 1985
- An experimental investigation of an airfoil undergoing large-amplitude pitching motionsAIAA Journal, 1985
- Experimental investigation of dynamic stall for a pitching airfoilJournal of Aircraft, 1984
- Dynamic Stall Experiments on Oscillating AirfoilsAIAA Journal, 1976
- Dynamic Stall Considerations in Helicopter RotorsJournal of the American Helicopter Society, 1968