Numerical simulation of a controlled-flow tunnel for V/STOL testing
- 1 March 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (3) , 186-191
- https://doi.org/10.2514/3.45287
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Adaptable wind tunnel for testing V/STOL configurations at high liftJournal of Aircraft, 1983
- Interference-Free Wind-Tunnel Flows by Adaptive-Wall TechnologyJournal of Aircraft, 1977
- A theory of the jet flap in three dimensionsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959
- The lift coefficient of a thin, jet-flapped wingProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1956