Exact Method of Designing Airfoils With Given Velocity Distribution in Incompressible Flow
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (11), 651-659
- https://doi.org/10.2514/3.60278
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- A class of airfoils designed for high lift in incompressible flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Optimization of airfoils for maximum liftJournal of Aircraft, 1970
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959