https://doi.org/10.1140/epjp/s13360-023-04827-z
Regular Article
Aerodynamic performance improvement of an airfoil using the Gurney flap and fast on–off DBD plasma actuator
1
Faculty of Mechanical Engineering, University of Guilan, Rasht, Iran
2
Faculty of Technology and Engineering, East of Guilan, University of Guilan, Rudsar, Iran
Received:
8
August
2023
Accepted:
22
December
2023
Published online:
7
January
2024
This study is focused on proposing a novel configuration by simultaneous utilization of Gurney flap and DBD plasma actuator on a NACA 0012 wind turbine airfoil for the purpose of flow control and aerodynamic performance improvement. In this regard, the airfoils with different Gurney flap and DBD plasma actuator configurations are examined by means of numerical simulations. Also, the effective range of the Gurney flap and DBD plasma actuator based on the AoA on the aerodynamic performance improvement is determined. The results indicate that compared to a clean airfoil, attaching the Gurney flap and DBD plasma actuator results in an improvement in the lift coefficient. It is evident that the drag coefficient, especially at the angles of attack higher than 6°, is sensitive to the position of the DBD plasma (XP). The results illustrate that the airfoil equipped with the Gurney flap and the DBD plasma at XP = 0.25 C is best suited to improve the ratio of lift to drag and aerodynamic performance. Hence, for the angle of attack values less than 6°, the DBD plasma actuator must be turned off, and at higher angle of attack values, the DBD plasma actuator must be switched on.
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© The Author(s), under exclusive licence to Società Italiana di Fisica and Springer-Verlag GmbH Germany, part of Springer Nature 2024. Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.