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Cited article:

The effects of actuation frequency on the separation control over an airfoil using a synthetic jet

Y. Abe, K. Okada, T. Nonomura, K. Fujii

Published online: 2015-06-08

DOI: https://doi.org/10.1051/eucass/201507147

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This article has been cited by the following article(s):

Burst-Mode Frequency Effects of Dielectric Barrier Discharge Plasma Actuator for Separation Control

Satoshi Sekimoto, Taku Nonomura and Kozo Fujii
AIAA Journal 55 (4) 1385 (2017)
DOI: 10.2514/1.J054678
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Lagrangian analysis of mass transport and its influence on the lift enhancement in a flow over the airfoil with a synthetic jet

Shengli Cao, Ya Li, Jiazhong Zhang and Yoshihiro Deguchi
Aerospace Science and Technology 86 11 (2019)
DOI: 10.1016/j.ast.2019.01.008
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Three Flow Features behind the Flow Control Authority of DBD Plasma Actuator: Result of High-Fidelity Simulations and the Related Experiments

Kozo Fujii
Applied Sciences 8 (4) 546 (2018)
DOI: 10.3390/app8040546
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