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Energies 2020, 13, 1374 19 of 20 12. Kelley, C.L.; Bowles, P.O.; Cooney, J.; He, C.; Corke, T.C.; Osborne, B.A.; Silkey, J.S.; Zehnle, J. Leading-edge separation control using alternating-current and nanosecond-pulse plasma actuators. AIAA J. 2014, 52, 1871–1884. [CrossRef] 13. Corke, T.; Mertz, B.; Patel, M. Plasma flow control optimized airfoil. In Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA, 9–12 January 2006; p. 1208. 14. Thomas, F.O.; Corke, T.C.; Iqbal, M.; Kozlov, A.; Schatzman, D. Optimization of dielectric barrier discharge plasma actuators for active aerodynamic flow control. AIAA J. 2009, 47, 2169. [CrossRef] 15. Forte, M.; Jolibois, J.; Pons, J.; Moreau, E.; Touchard, G.; Cazalens, M. Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: Application to airflow control. Exp. Fluids 2007, 43, 917–928. [CrossRef] 16. Wang, C.C.; Durscher, R.; Roy, S. Three-dimensional effects of curved plasma actuators in quiescent air. J. Appl. Phys. 2011, 109, 083305. [CrossRef] 17. Belan, M.; Messanelli, F. Compared ionic wind measurements on multi-tip corona and DBD plasma actuators. J. Electrost. 2015, 76, 278–287. [CrossRef] 18. Messanelli, F.; Belan, M. Ionic wind measurements on multi-tip plasma actuators. In Proceedings of the EFM15—Experimental Fluid Mechanics 2015, Prague, Czech Republic, 17–20 November 2015; pp. 1–8. 19. Messanelli, F.; Belan, M. A comparison between corona and DBD plasma actuators for separation control on an airfoil. In Proceedings of the 55th AIAA Aerospace Sciences Meeting, Grapevine, TX, USA, 9–13 January 2017; p. 0395. 20. Messanelli, F.; Frigerio, E.; Tescaroli, E.; Belan, M. Separation control by plasma actuators: Effects of direct momentum injectionandvortexgeneration. FlowTurbulenceCombust.2019.[CrossRef] 21. Zoppini, G.; Di Vinci, L.; Campanardi, G.; Zanotti, A.; Belan, M. PIV characterization of a separated flow controlled by a DBD actuator. In Proceedings of the XXVI AIVELA National Meeting, Milano, Italy, 29–30 November 2018; pp. 1–13. 22. Corke, T.; Enloe, C.; Wilkinson, S. Dielectric barrier discharge plasma actuators for flow control. Ann. Rev. Fluid Mech. 2010, 42, 505–529. [CrossRef] 23. Winkelmann, A. Flow field studies behind a wing at low reynolds numbers. In Proceedings of the AIAA 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference, Seattle, WA, USA, 18–20 June 1990; pp. 1–18. 24. Winkelmann, A.; Barlow, J. A flowfield model for a rectangular planform wing beyond stall. AIAA J. 1980, 18, 1006–1008. [CrossRef] 25. Boiko, A.; Dovgal, A.; Zanin, B.; Kozlov, V. Three-dimensional structure of separated flows on wings (review). Thermophys. Aeromech. 1996, 3, 1–13. 26. Wicks, M.; Thomas, F.O.; Corke, T.C.; Patel, M.; Cain, A.B. Mechanism of vorticity generation in plasma streamwise vortex generators. AIAA J. 2015, 53, 3404–3413. [CrossRef] 27. Belan, M.; Messanelli, F. Wind tunnel testing of multi-tip corona actuators on a symmetric airfoil. J. Electrost. 2017, 85, 23–34. 28. Messanelli, F.; Frigerio, E.; Tescaroli, E.; Belan, M. Flow separation control by pulsed corona actuators. Exp. Therm. Fluid Sci. 2019, 105, 123–135. [CrossRef] 29. Messanelli, F. Optimization of plasma actuators for flow control. Ph.D. Thesis, Politecnico di Milano, Milano, Italy, 2017. [CrossRef] 30. Kriegseis, J.; Grundmann, S.; Tropea, C. Performance reduction of dielectric barrier discharge plasma actuators at higher mach numbers. In New Results in Numerical and Experimental Fluid Mechanics VIII; Springer: Berlin/Heidelberg, Germany 2013; pp. 209–217. [CrossRef] 31. Jukes, T.N.; Choi, K.S. On the formation of streamwise vortices by plasma vortex generators. J. Fluid Mech. 2013, 733, 370–393. 32. Auteri, F.; Carini, M.; Zagaglia, D.; Montagnani, D.; Gibertini, G.; Merz, C.; Zanotti, A. A novel approach for reconstructing pressure from PIV velocity measurements. Exp. Fluids 2015, 56, 45.PDF Image | Stall Control by Plasma Actuators: Characterization along the Airfoil Span
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