Multi-Electrode Plasma Actuator to Improve Performance of Flow Separation Control-Reference-Cited by-同舟云学术

Multi-Electrode Plasma Actuator to Improve Performance of Flow Separation Control

Published:2017 Issue:1 Volume:9 Page:1-8
ISSN:1882-5079
Container-title:International Journal of Gas Turbine, Propulsion and Power Systems
language:en
Short-container-title:JGPP

Author:

Asaumi Norio¹²,Matsuno Shinsuke¹,Matsuno Takashi²,Sugahara Masataka²,Kawazoe Hiromitsu²

Affiliation:

1. IHI Corporation

2. Department of Mechanical and Aerospace Engineering, Tottori University

Publisher

Gas Turbine Society of Japan

Subject

Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/jgpp/9/1/9_1/_pdf

Reference14 articles.

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2. Corke, T. C., Post, M. L., and Orlov, D. M., 2007, “SDBD Plasma Enhanced Aerodynamics: Concepts, Optimization and Applications,” Progress in Aerospace Sciences , Vol. 43, No. 7 7-8, pp. 193 193-217.

3. Font, G. I., and Morgan, W. L., 2007, “Recent Progress in Dielectric Barrier Discharges for Aerodynamic Flow Control,” Contributions to Plasma Physics , Vol. 47, No. 1 1-2, pp.103-110.

4. Matsuno, T., Maeda, K., Yamada, G., Kawazoe, H. and KanKanazaki, M. M., 2013, “Improvement of Flow Control Performance of Plasma Actuator Using Wind-Tunnel Test Based Efficient Global Optimization,” 31st AIAA Applied Aerodynamics Conference Conference, AIAA 2013-2512.

5. Forte, M., Jolibois, J., Pons, J., Moreau, E., Touchard, G., and Cazalens, M., 2007, “Optimization of a Dielectric Barrier Discharge Actuator by Statio nary and Non-Stationary Measurements of the Induced Flow Velocity:Application to airflow control,” Experiments in Fluids , Vol. 43, pp pp.917-928.

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