Overview of Plasma Flow Control: Concepts, Optimization, and Applications
By Thomas C. Corke, Martiqua L. Post. 2005
283 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Applied Mathematics, Electrical and Electronic Engineering
View Paper: https://www.semanticscholar.org/paper/01f46e380d905a5a351d6c9a97dcc141928fd701
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Eric Moreau
- N. Benard
- Marios Kotsonis
- Venkat Narayanaswamy
- Gérard Touchard
- J. Jolibois
- M. Forte
- M. Cazalens
In Applied Mathematics
In Electrical and Electronic Engineering
Citations in the corpus
- Airflow control by non-thermal plasma actuators (2007, result): “Concerning flow control over an oscillating airfoil, all the results may be found in [127,128,130] which consist of a summary of previous works.”
- Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control (2007, background): “More recently, some works performed by Post and Corke (2004) and Corke and Post (2005) with NACA airfoils have shown lift improvement in stall configurations.”
- Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, background): “…eric.moreau@univ-poitiers.fr Exp Fluids (2014) 55:1846 1 3 1846 Page 2 of 43 manipulate the dynamics of different flows, such as separated flows (Corke and Post 2005; Little and Samimy 2010; McLaughlin et al. 2006; Benard and Moreau 2011; Kelley et al. 2012; Jukes and Choi 2009), developing…”
- Strategies for control of transitional and turbulent flows using plasma-based actuators (2006, methodology): “In order to reduce power consumption, the actuator may be operated in a pulsed manner, as described in Corke and Post (2005).”
- Characterization of a High-Frequency Pulsed-Plasma Jet Actuator for Supersonic Flow Control (2010, methodology): “DBD plasma actuators have been successfully used for separation control on flat plates [2,3], bluff bodies [4,5], and airfoils [6,7] and to inducemixing enhancement of jets [8].”