Plasma Flaps and Slats: An Application of Weakly Ionized Plasma Actuators

By Chuan He, Thomas C. Corke, Mehul P. Patel. 2004

307 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/74d1fcaae8820419f1fb496e2298e0585ecdb2e3

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In Aerospace Engineering

In Computational Mechanics

Citations in the corpus

Scaling Effects of an Aerodynamic Plasma Actuator (2007, methodology): “This shape was chosen because it was the subject of earlier experiments on the control of steady and dynamic stall using plasma actuators [15,18,19].”
Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, background): “Then, a few research groups in the world started to study DBD plasma actuators and their ability to manipulate airflow (Corke and He 2004; Enloe et al. 2004a, b; Pons et al. 2004, 2005).”
High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “This results in a uniform increase in lift coefficient across all angles of attack and a slight reduction in minimum drag coefficient, CD, at Reynolds numbers on the order of 105 corresponding to velocities of a few tens of meters per second (He et al. 2009).”
Dielectric Barrier Discharge Plasma Actuators for Flow Control (2010, background): “2007, Visbal & Gaitonde 2006), and airfoil leading-edge separation control (Corke et al. 2004; Post 2004; Post & Corke 2003, 2004).”
Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications (2009, background): “As with other separated flows[8, 38], Thomas et al.”
Airflow control by non-thermal plasma actuators (2007, methodology): “During the same period as Corke et al in 2002, Sosa et al conducted the same kind of experiments, but the actuator was a surface corona-based one.”
Diagnostics for characterisation of plasma actuators (2015, background): “Their utilisation has been proposed, among others, for airfoil separation control [41–45], turbine blade separation control [46], laminar-turbulent transition delay [47], lift enhancement [48, 49], bluff body flow control [50, 51], shock wave control [52] and combustion augmentation [38].”