Downwash correction for a two-dimensional finite wing
- 1 September 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (9) , 745-746
- https://doi.org/10.2514/3.44301
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Calculation Method for Circulation Control by Tangential Blowing Around a Bluff Trailing EdgeAeronautical Quarterly, 1968
- An Experimental Investigation of a Low-Speed Circulation-Controlled AerofoilAeronautical Quarterly, 1968