Experiments with an adaptable-wall wind tunnel for large lift
- 1 June 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (6) , 371-376
- https://doi.org/10.2514/3.45455
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Numerical simulation of a controlled-flow tunnel for V/STOL testingJournal of Aircraft, 1986
- A review of adaptive wall wind tunnelsProgress in Aerospace Sciences, 1985
- Adaptable wind tunnel for testing V/STOL configurations at high liftJournal of Aircraft, 1983
- Adaptive-wall wind-tunnel development for transonic testingJournal of Aircraft, 1981
- Self correcting wind tunnelsThe Aeronautical Journal, 1974
- A method for transonic wind-tunnel corrections.AIAA Journal, 1973