Dynamic stall experiments on a swept three-dimensional wing in compressible flow
- 24 June 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Incipient torsional stall flutter aerodynamic experiments on a sweptthree-dimensional wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Compressible studies on dynamic stallPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Combined translation/pitch motion - A new airfoil dynamic stall simulationJournal of Aircraft, 1988
- Airfoil dynamic stall at constant pitch rate and high Reynolds numberJournal of Aircraft, 1988