'Spilled' leading-edge vortex effects on dynamic stall characteristics
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (4) , 313-315
- https://doi.org/10.2514/3.44527
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Dynamic Effects of Shock-Induced Flow SeparationJournal of Aircraft, 1975
- Dynamic stall experiments on oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Analytic prediction of dynamic stall characteristicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Dynamic Stall Considerations in Helicopter RotorsJournal of the American Helicopter Society, 1968