Development of advanced circulation control wing high-lift airfoils
- 1 July 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (7) , 476-483
- https://doi.org/10.2514/3.44996
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Design of the Circulation Control Wing STOL Demonstrator AircraftJournal of Aircraft, 1981
- Flight testing the circulation control wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979