A General Class of Exact Airfoil Solutions
- 1 August 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (8) , 574-580
- https://doi.org/10.2514/3.59038
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Optimization of airfoils for maximum liftJournal of Aircraft, 1970
- XLII. A new family of wing profilesJournal of Computers in Education, 1937