Adaptable wind tunnel for testing V/STOL configurations at high lift
- 1 November 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (11) , 968-974
- https://doi.org/10.2514/3.48200
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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