Control of trailing-edge noise from airfoil using a plasma actuator-Reference-Cited by-同舟云学术

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Control of trailing-edge noise from airfoil using a plasma actuator

Published:2018 Issue:1 Volume:13 Page:JFST0003-JFST0003
ISSN:1880-5558
Container-title:Journal of Fluid Science and Technology
language:en
Short-container-title:JFST

Author:

INASAWA Ayumu¹,KAGAWA Yui¹

Affiliation:

1. Department of Aerospace Engineering, Tokyo Metropolitan University

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/jfst/13/1/13_2018jfst0003/_pdf

Reference17 articles.

1. Akishita, S., Tone-like noise from an isolated two dimensional airfoil, AIAA paper, (1986), AIAA-86-1947.

2. Arbey H. and Bataille J., Noise generated by airfoil profiles placed in a uniform laminar flow, Journal of Fluid Mechanics, Vol. 134, (1983), pp. 33-47.

3. Corke, T.C., Enloe, C.L. and Wilkinson, S.P., Dielectric barrier discharge plasma actuators for flow control, Annual Review of Fluid Mechanics, Vol. 42, (2010), pp. 505-529.

4. Desquesnes, M., Terracol M. and Sagaut P., Numerical investigation of the tone noise mechanism over laminar airfoils, Journal of Fluid Mechanics, Vol. 591, (2007), pp. 155-182.

5. Fink, M.R., Prediction of airfoil tone frequencies, Journal of Aircraft, Vol. 12, No. 2, (1975), pp.118-120.

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