Multiple element airfoils optimized for maximum lift coefficient.
- 1 December 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (12), 1620-1624
- https://doi.org/10.2514/3.6694
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Optimization of airfoils for maximum liftJournal of Aircraft, 1970
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959