Numerical simulation for control effect of backward-facing step flow by a plasma actuator with burst modulation

Author:

LEE Keunseob1,KIKUCHI Satoshi1,IMAO Shigeki1

Affiliation:

1. Department of Mechanical Engineering, Gifu University

Publisher

Japan Society of Mechanical Engineers

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), DOI:10.2514/6.2006-369.

2. Barkley, D., Gomes, M. G. M. and Henderson, R. D., Three-dimensional instability in flow over a backward-facing step, Journal of Fluid Mechanics, Vol. 473 (2002), pp.167–190.

3. Chun, K.B. and Sung, H. J., Control of turbulent separated flow over a backward-facing step by local forcing, Experiments in Fluids, Vol. 21 (1996), pp.505–529.

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. Ffowcs-Williams, J.E. and Zhao, B.C., The active control of vortex shedding, Journal of Fluids and Structures, Vol. 3 (1989), pp.115–122.

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