Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift
- 1 November 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (11) , 920-925
- https://doi.org/10.2514/3.57581
Abstract
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