Wyszukiwarka
Enhancement of lift and drag performances of a NACA0012 airfoil by multi-DBD plasma actuator with additional floating interelectrodes
Abstrakt
It is clear that the improvement of aircraft aerodynamic performances is currently and will continue to be a significant area of research for the aeronautical industry. The current study is focused on theenhancement of aerodynamic airfoil performances by using a multi-DBD plasma actuator mounted around the model leading-edge. Experiments have been conducted at the University of Orleans, in the 2 m x 2 m test section of a large wind tunnel in which a NACA0012 airfoil was mounted in a 2D flow configuration. Tests have been carried out in a velocity range of 10 - 40 m.s-1, resulting in Reynolds numbers based on the chord length of 200,000 ≤ Re ≤ 800,000. The actuator consisted of copper electrodes flush mounted with an asymmetric disposition on both sides of a dielectric panel constituted by four layers of Kapton® tape, and with saw-like grounded electrodes and floating inter-electrodes. This multi-DBD plasma actuator ensures a thinwall jet produced tangentially to the dielectric surface and continuously accelerated along the successive discharges. Aerodynamic load measurements and Particle Image Velocimetry have been performed to characterize the benefits of the control. Results show potentialities of such actuator to delay stall configuration and to enhance lift in a full post-stall separated flow.
Autorzy (6)
Cytuj jako
Pełna treść
pełna treść publikacji nie jest dostępna w portalu
Słowa kluczowe
Informacje szczegółowe
- Kategoria:
- Aktywność konferencyjna
- Typ:
- publikacja w wydawnictwie zbiorowym recenzowanym (także w materiałach konferencyjnych)
- Tytuł wydania:
- Proceedings of the International Symposium on Electrohydrodynamics,Gdańsk, Poland, September 23-26, 2012 strony 67 - 72
- Język:
- angielski
- Rok wydania:
- 2012
- Opis bibliograficzny:
- Leroy A., Audier P., Podlinski J., Berendt A., Hong D., Mizeraczyk J.: Enhancement of lift and drag performances of a NACA0012 airfoil by multi-DBD plasma actuator with additional floating interelectrodes// Proceedings of the International Symposium on Electrohydrodynamics,Gdańsk, Poland, September 23-26, 2012/ ed. eds. K. Garasz, M. Dors. : , 2012, s.67-72
- Weryfikacja:
- Politechnika Gdańska
wyświetlono 45 razy
Publikacje, które mogą cię zainteresować
Fully Separated Flow Control Using DBD Plasma Actuators Located at the Leading Edge of an Airfoil
- A. Leroy,
- P. Audier,
- D. Hong
- + 3 autorów
Trailing-Edge Separation Control of a NACA 0015 Airfoil Using Dielectric-Barrier-Discharge Plasma Actuators
- R. D. Whalley,
- A. Debien,
- J. Podliński
- + 6 autorów