Effect of compressibility on dynamic stall of a pitching airfoil
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Viscous Transonic Airfoil Workshop compendium of resultsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Dynamic Effects of Shock-Induced Flow SeparationJournal of Aircraft, 1975