Aerodynamic characteristics of a circulation control elliptical airfoil with two blown jets
- 1 September 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (9) , 737-742
- https://doi.org/10.2514/3.45195
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Circulation controlled STOL wing optimizationJournal of Aircraft, 1984
- Wind-Tunnel Study of a Circulatis Elliptical AirfoiJournal of Aircraft, 1977
- Two-Dimensional Subsonic Wind Tunnel Evaluation of Two Related Cambered 15-Percent Thick Circulation Control AirfoilsPublished by Defense Technical Information Center (DTIC) ,1977
- Flight Performance of a Circulation Controlled STOL AircraftJournal of Aircraft, 1976
- Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1975
- Two Dimensional Subsonic Wind Tunnel Tests on a 20 Percent Thick, 5 Percent Cambered Circulation Control AirfoilPublished by Defense Technical Information Center (DTIC) ,1970
- An Experimental Investigation of a Low-Speed Circulation-Controlled AerofoilAeronautical Quarterly, 1968