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Development of DBD plasma actuators: The double encapsulated electrode

Journal

ACTA ASTRONAUTICA
Volume 109, Issue -, Pages 132-143

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2014.12.016

Keywords

Plasma actuator; Dielectric barrier discharge

Funding

  1. Engineering and Physical Sciences Research Council (EPSRC) [EP/H5000154/1]

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Plasma actuators are electrical devices that generate a wall bounded jet without the use of any moving parts. For aerodynamic applications they can be used as flow control devices to delay separation and augment lift on a wing. The standard plasma actuator consists of a single encapsulated (ground) electrode. The aim of this project is to investigate the effect of varying the number and distribution of encapsulated electrodes in the dielectric layer. Utilising a transformer cascade, a variety of input voltages are studied for their effect. In the quiescent environment of a Faraday cage the velocity flow field is recorded using particle image velocimetry. Through understanding of the mechanisms involved in producing the wall jet and the importance of the encapsulated electrode a novel actuator design is proposed. The actuator design distributes the encapsulated electrode throughout the dielectric layer. The experiments have shown that actuators with a shallow initial encapsulated electrode induce velocities greater than the baseline case at the same voltage. Actuators with a deep initial encapsulated electrode are able to induce the highest velocities as they can operate at higher voltages without breakdown of the dielectric. (C) 2015 IAA. Published by Elsevier Ltd. on behalf of IAA. This is an open access article under the CC BY license (http://creativecommons.org/licenses/by/4.0/).

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