A Class of Airfoils Designed for High Lift in Incompressible Flow
- 1 October 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (10) , 610-617
- https://doi.org/10.2514/3.60268
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Multiple element airfoils optimized for maximum lift coefficient.AIAA Journal, 1972
- Optimization of airfoils for maximum liftJournal of Aircraft, 1970
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959
- An experimental flow with zero skin friction throughout its region of pressure riseJournal of Fluid Mechanics, 1959