LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 13.1-PERCENT-THICK, HIGH-LIFT AIRFOIL
- 1 February 1974
- conference paper
- Published by SAE International in SAE Technical Paper Series
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A Class of Airfoils Designed for High Lift in Incompressible FlowJournal of Aircraft, 1973
- Multiple element airfoils optimized for maximum lift coefficient.AIAA Journal, 1972
- Mathematical model for two-dimensional multi-component airfoils in viscous flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Optimization of airfoils for maximum liftJournal of Aircraft, 1970
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959