Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control
By M. Forte, J. Jolibois, J. Pons, Eric Moreau, Gérard Touchard, M. Cazalens. 2007
542 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/eebbb7aaa7fd06ee75a3fb92275baafafc7fcf3b
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
- Marios Kotsonis
- Eric Moreau
- Igor V. Adamovich
- N. Benard
- Thomas C. Corke
- Martiqua L. Post
- Mohammad Samimy
- J. Little
In Electrical and Electronic Engineering
- Marios Kotsonis
- Eric Moreau
- N. Benard
- Igor V. Adamovich
- Thomas C. Corke
- J. Little
- Mohammad Samimy
- M. Nishihara
In Radiology, Nuclear Medicine and Imaging
- Marios Kotsonis
- Eric Moreau
- N. Benard
- Thomas C. Corke
- Igor V. Adamovich
- J. Little
- M. Nishihara
- Mohammad Samimy
Citations in the corpus
- Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications (2009, methodology): “ Forte et al. (2006) experimentally examined the effect of the amount of overlap between the bare and covered electrodes in an asymmetric arrangement like that in Fig. 1. They defined the gap spacing, g, to be positive when there was a non-overlaping distance between the edges.”
- Diagnostics for characterisation of plasma actuators (2015, methodology): “Although the technique has been used in some studies [64, 77, 112, 118, 159], the accuracy problems previously mentioned regarding Figure 24.”
- Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control (2014, methodology): “In Forte et al. (2006), velocity measurements for glass (εr = 10) and PMMA (εr = 3) materials are compared.”
- High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “20 in)) between exposed and covered electrodes (Roth and Dai 2006; Forte et al. 2007).”
- Streamer inhibition for improving force and electric wind produced by DBD actuators (2012, background): “The discharge induced during the positive and negative going-cycles of one ac sine period exhibits two different plasma regimes [3, 4–6].”
- Electric wind produced by surface plasma actuators: a new dielectric barrier discharge based on a three-electrode geometry (2008, unknown): “In agreement with previous works [26,28], this shows that the electric wind velocity increases with the applied AC HV.”
- Airflow control by non-thermal plasma actuators (2007, methodology): “In the next study [77], Forte et al performed the same kind of measurements, but they were now able to synchronize the records of the voltage, the current and the velocity (xcomponent and y-component).”
- Measurement of the body force field of plasma actuators (2011, background): “Several studies focus on the investigation of the induced velocity field [18, 19, 20] and the produced thrust from the actuators [21, 22, 23].”