Lift Enhancement of an Airfoil and an Unmanned Aerial Vehicle by Plasma Gurney Flaps
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics, 100191 Beijing, People’s Republic of China
2. Beijing Institute of Mechanical Equipment, 100854 Beijing, People’s Republic of China
Funder
Fundamental Research Funds for the Central Universities of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055426
Reference25 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. Gurney flap—Lift enhancement, mechanisms and applications
3. Comparisons of a Gurney and Jet-Flap for Hinge-Less Control
4. Attenuation of Tollmien–Schlichting Waves Using Plasma Actuator Vortex Generators
5. Influence of circulation on a rounded-trailing-edge airfoil using plasma actuators
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