Asymmetric surface dielectric barrier discharge in air at atmospheric pressure: electrical properties and induced airflow characteristics

By J. Pons, Eric Moreau, Gérard Touchard. 2005

340 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering, Radiology, Nuclear Medicine and Imaging

View Paper: https://www.semanticscholar.org/paper/9cd6de754358f2abbe1ac4c9af2e4b61ea370304

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In Aerospace Engineering

In Electrical and Electronic Engineering

In Radiology, Nuclear Medicine and Imaging

Citations in the corpus

Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, methodology): “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).”
Streamer inhibition for improving force and electric wind produced by DBD actuators (2012, background): “negative going-cycle, as experimentally highlighted in [5] for instance.”
Electrohydrodynamic force in dielectric barrier discharge plasma actuators (2007, background): “[4]), the EHD force extends over several mm along and above the dielectric surface.”
Diagnostics for characterisation of plasma actuators (2015, methodology): “In order to bypass the resolution problems of direct current measurements, integral charge measurement techniques can be used [68, 86, 146, 161, 162] for power estimation.”
Experimental study of a DBD surface discharge for the active control of subsonic airflow (2008, methodology): “Pons et al [29] also observed this difference and optical measurements using a photomultiplier tube showed that these two discharges are slightly different from the point of view of light emission [26].”
Electrostatic cleaning system for removal of sand from solar panels (2013, methodology): “Based on this investigation, we are developing an optional technology to enhance the cleaning by utilizing natural wind or by applying forced convection using a plasma actuator that generates electrostatic wind [8,9].”
High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “It should be noted that other methods for this calculation have been suggested, but a widely accepted standard for plasma actuators does not exist to the authors’ knowledge (Pons et al. 2005; Porter et al. 2007; Greenblatt et al. 2008a; Hoskinson et al. 2008).”
Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control (2007, methodology): “The higher the voltage is, the further the plasma area extends and some previous works have shown that the maximum velocity position is at the end of the plasma area (Pons et al. 2005).”