Control of dynamic flowfield around a pitching NACA633−618 airfoil by a DBD plasma actuator

Author:

Fukumoto Hiroaki,Aono Hikaru,Watanabe TakeshiORCID,Tanaka Motofumi,Matsuda Hisashi,Osako Toshiki,Nonomura TakuORCID,Oyama Akira,Fujii Kozo

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference67 articles.

1. Efficient evaluations of symmetric-conservative metrics for high-order finite-difference scheme on a rotating grid;Abe,2015

2. Scalar tuning of a fluid solver using compact scheme for a supercomputer with a distributed memory architecture;Aono;CFD Letters,2013

3. Effects of burst frequency and momentum coefficient of DBD actuator on control of deep-stall flow around NACA0015 at Rec=2.6×105;Aono,2014

4. Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air;Aono;Mech. Eng. J.,2015

5. Les of transient flows controlled by DBD plasma actuator over a stalled airfoil;Asada;Int. J. Comut. Fluid Dyn,2015

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