Flow Control with Electrohydrodynamic Actuators

By G. Artana, Juan D’Adamo, L. Léger, Eric Moreau, Gérard Touchard. 2001

139 citations recorded by the source corpus.

Subfields: Electrical and Electronic Engineering, Materials Chemistry

View Paper: https://www.semanticscholar.org/paper/663093a1e336b39d91180cbc208d09fa857729e9

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In Electrical and Electronic Engineering

In Materials Chemistry

Citations in the corpus

Active control of high-speed and high-Reynolds-number jets using plasma actuators (2005, result): “This is consistent with experimental results on EHD airfoil flow separation control, demonstrated at U∞ ∼ 1–10 m s−1 (Roth, Sherman & Wilkinson 2000; Corke & Matlis 2000; Artana et al. 2002), U∞ ∼ 10–30 m s−1 (Post & Corke 2004), and U∞ ∼ 20– 75 m s−1 (Zavialov et al.”
Development and use of localized arc filament plasma actuators for high-speed flow control (2007, unknown): “∂t + 1 r ∂(ρur) ∂r = 0, ( 4 ) ρ ∂u ∂t + ρu ∂u ∂r = ∂ ∂r µ r ∂(ur) ∂r − ∂P ∂r , (5)”
Electric wind produced by surface plasma actuators: a new dielectric barrier discharge based on a three-electrode geometry (2008, unknown): “This group includes the DC surface discharges [3, 4, 17, 25], the surface dielectric barrier discharges [26–29] and the travelling wave surface discharges [1, 30, 31].”
Development and characterization of plasma actuators for high-speed jet control (2004, background): “…control mainly focus on viscous drag reduction 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…”
Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control (2007, background): “(2002) or Artana et al. (2002). The study related to the present paper has focused on the single DBD actuator which is presented in Fig.”
Airflow control by non-thermal plasma actuators (2007, background): “For instance, in [28], a dc-energized wire-toplane actuator placed at the leading edge of a flat plate parallel to the free air stream allowed them to increase significantly the velocity inside the boundary layer, up to 10 m s−1 at U∞ = 17.”
Diagnostics for characterisation of plasma actuators (2015, methodology): “The majority of studies on DC-corona actuators have since been published mainly by the group of University of Poitiers, France and the group of University of Buenos Aires, Argentina [5, 21].”