Wind-Tunnel Study of a Circulatis Elliptical Airfoi
- 1 September 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (9) , 881-886
- https://doi.org/10.2514/3.58868
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Boundary-Layer TheoryPublished by Springer Nature ,2000
- Flight Performance of a Circulation Controlled STOL AircraftJournal of Aircraft, 1976
- Circulation Control for High Lift and Drag Generation on STOL AircraftJournal of Aircraft, 1975
- Downwash correction for a two-dimensional finite wingJournal of Aircraft, 1971
- Two-Dimensional Transonic Wind Tunnel Tests of Three 15-Percent Thick Circulation Control AirfoilsPublished by Defense Technical Information Center (DTIC) ,1970
- 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