Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators

By Martiqua L. Post, Thomas C. Corke. 2004

688 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/72c9d4ffd4df4a700ff78cd4efe07aad1e43a32c

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In Aerospace Engineering

In Computational Mechanics

Citations in the corpus

Active control of a Mach 0.9 jet for noise mitigation using plasma actuators (2007, background): “Note that the nature of a hightemperature, localized arc discharge is completely different from low-temperature, low-current, diffuse glow discharges used in previous low-speed flow control work [49,50].”
Development and characterization of plasma actuators for high-speed jet control (2004, background): “…and control of boundary layer separation in subsonic flows (Roth et al. 2000; Corke and Matlis 2000; Artana et al. 2001; Leonov et al. 2001; Post and Corke 2003), shock wave modification and wave drag reduction in supersonic and hypersonic flows (Tret’yakov et al. 1996; Minucci et al.…”
Scaling Effects of an Aerodynamic Plasma Actuator (2007, methodology): “[15] (right), and b) visualized flow around the airfoil at 16 degwith leading-edge plasma actuator”
Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications (2009, methodology): “With a similar intent, Cavalieri[6] and Corke et al.[7] used an University of Notre Dame Center for Flow Physics and Control azimuthal array of plasma actuators on the surface of a sharp-tipped circular cone in a Mach 3.5 flow.”
Active control of high-speed and high-Reynolds-number jets using plasma actuators (2005, background): “The high-current, high-temperature, localized arc discharge is completely different from low-temperature, low-current, diffuse glow discharges used in previous low-speed flow control work (Roth et al.; Wilkinson 2000; Post & Corke 2004).”
High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “Early examples of plasma actuators as flow control devices demonstrated their potential for boundary layer and leading edge airfoil separation control applications (Roth et al. 2000; Post and Corke 2004).”
Strategies for control of transitional and turbulent flows using plasma-based actuators (2006, background): “Velocity measurements (Post and Corke 2003 ) indicate that the averaged plasma-induced body force results is the formation of a wall jet.”
Separation Control Using Plasma Actuators: Dynamic Stall Vortex Control on Oscillating Airfoil (2006, methodology): “Details of the airfoil’s manufacturing process can be found in Post and Corke [24].”
Plasma Flaps and Slats: An Application of Weakly Ionized Plasma Actuators (2004, methodology): “mean velocity distribution produced by this actuator arrangement [14].”