Design of the Circulation Control Wing STOL Demonstrator Aircraft
- 1 January 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (1) , 51-58
- https://doi.org/10.2514/3.57463
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- STOE Potential of the Circulation Control Wing for High-Performance AircraftJournal of Aircraft, 1978
- Circulation Control for High Lift and Drag Generation on STOL AircraftJournal of Aircraft, 1975