Circulation controlled STOL wing optimization
- 1 February 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (2) , 128-134
- https://doi.org/10.2514/3.48235
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Flight Performance of a Circulation Controlled STOL AircraftJournal of Aircraft, 1976
- Thrust augmented wing sections in transition flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Accurate Numerical Methods for Boundary-Layer Flows. II: Two Dimensional Turbulent FlowsAIAA Journal, 1972
- An Experimental Investigation of a Low-Speed Circulation-Controlled AerofoilAeronautical Quarterly, 1968