Further Consideration of ''Spilled" Leading-Edge Vortex Effects on Dynamic Stall
- 1 June 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (6) , 601-603
- https://doi.org/10.2514/3.58827
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Dynamic Stall Analysis in Light of Recent Numerical and Experimental ResultsJournal of Aircraft, 1976
- 'Spilled' leading-edge vortex effects on dynamic stall characteristicsJournal of Aircraft, 1976
- Dynamic Stall Experiments on Oscillating AirfoilsAIAA Journal, 1976
- Unsteady Airfoil Stall, Review and ExtensionJournal of Aircraft, 1971
- Dynamic Stall Simulation ProblemsJournal of Aircraft, 1971
- Dynamic Stall Considerations in Helicopter RotorsJournal of the American Helicopter Society, 1968
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938