Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control-Reference-Cited by-同舟云学术

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Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control

Published:2015-09 Issue:9 Volume:53 Page:2544-2559
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Sato Makoto¹,Aono Hikaru¹,Yakeno Aiko¹,Nonomura Taku¹,Fujii Kozo¹,Okada Koichi²,Asada Kengo³

Affiliation:

1. Department of Space Flight Systems, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan

2. Engineering Solution Division, Ryoyu Systems Company, Ltd., Nagoya 455-0024, Japan

3. Department of Aeronautics and Astronautics, University of Tokyo, Sagamihara 252-5210, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053700

Reference68 articles.

1. The control of flow separation by periodic excitation

2. AERODYNAMICS OF SMALL VEHICLES

3. SYNTHETIC JETS

4. Dielectric Barrier Discharge Plasma Actuators for Flow Control

5. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators

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