DBD Plasma actuator effect on a 2D model laminar boundary layer. Transition delay under ionic wind effect.-Reference-Cited by-同舟云学术

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DBD Plasma actuator effect on a 2D model laminar boundary layer. Transition delay under ionic wind effect.

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Seraudie Alain¹,Vermeersch O¹,Arnal D¹

Affiliation:

1. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3515

Reference9 articles.

1. Effect of Plasma Actuators on a Flat Plate Laminar Boundary Layer in Subsonic Conditions

2. A. Séraudie : `Implementation of plasma actuators ona flat plate. Effect of ionic wind on laminar-turbulent transition', 43ème Colloqued'Aérodynamique Appliquée 3AF- Poitiers10-12Mars2008.

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