Experimental Investigation of Aerodynamic Interactions of a Wing with Deployed Fowler Flap under Influence of a Propeller Slipstream
Author:
Affiliation:
1. Technische Universiteit Delft Faculteit Luchtvaart- en Ruimtevaarttechniek
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3216
Reference28 articles.
1. Design of the Cruise and Flap Airfoil for the X-57 Maxwell Distributed Electric Propulsion Aircraft
2. Drag Reduction Through Distributed Electric Propulsion
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