Surface velocity model of the flow caused by a DBD plasma actuator
Author:
Affiliation:
1. Department of Mechanical Engineering, Gifu University
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/85/869/85_18-00368/_pdf
Reference20 articles.
1. Anderson, R. and Roy, S., Preliminary experiments of barrier discharge plasma actuators using dry and humid air, American Institute of Aeronautics and Astronautics Paper, 2006-369 (2006).
2. Anzai, Y., Fukagata, K., Meliga, P., Boujo, E. and Gallaire, F., Numerical simulation and sensitivity analysis of a low-Reynolds-number flow around a square cylinder controlled using plasma actuators, Physical Review Fluids, Vol. 2 (2017), 043901.
3. Asada, K. and Fujii, K., Computational analysis of unsteady flow-field induced by plasma actuator in burst mode, 5th Flow Control Conference Chicago, Illinois (2010).
4. Corke, T., Jumper, E., Post, M., Orlov, D. and Mclaughlin, T., Application of weakly-ionized plasma as wing flow-control devices, American Institute of Aeronautics and Astronautics Paper, 2002-0350 (2002).
5. Igarashi, T., Naito, H. and Fukagata, K., Direct numerical simulation of flow around a circular cylinder, controlled using plasma actuators, Hindawi Publishing Corporation Mathematical Problems in Engineering, Vol. 2014 (2014), 591807, p.13．
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