Pitch rate and Reynolds number effects on a pitching rectangular wing
- 6 June 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Unsteady surface pressure measurements on a pitching rectangular wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Airfoil dynamic stall at constant pitch rate and high Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Visualization of dynamic stall controlled by large amplitude interrupted pitching motionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Visualization of three-dimensional forced unsteady separated flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Dynamic stall inception correlation for airfoils undergoing constantpitch rate motionsAIAA Journal, 1986
- 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
- [Back cover - Aug. 1985 [T-MTT]]IEEE Transactions on Microwave Theory and Techniques, 1985
- An experimental investigation of an airfoil undergoing large amplitude pitching motionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Water Tunnel Visualizations of Dynamic StallJournal of Fluids Engineering, 1979