Effect of Plasma-Based Control for Low-Reynolds Number Flapping Airfoil Performance-Reference-Cited by-同舟云学术

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Effect of Plasma-Based Control for Low-Reynolds Number Flapping Airfoil Performance

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Rizzetta Donald¹,Visbal Miguel¹

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-735

Reference75 articles.

1. Aerodynamics of Low Reynolds Number Flyers

2. PIV application in advanced low reynolds number facility

3. An Investigation of Low-Reynolds-Number Flows Past Airfoils

4. Comparison of Laminar Separation Bubble Measurements on a Low Reynolds Number Airfoil in Three Facilities

5. Numerical and Experimental Flow Analysis of Moving Airfoils with Laminar Separation Bubbles

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2. Control of Dynamically Stalled Flowfield around a Pitching Airfoil by DBD Plasma Actuator;8th AIAA Flow Control Conference;2016-06-10

3. Delay of Finite-Span Excrescence-Induced Transition Using Plasma-Based Control;7th AIAA Flow Control Conference;2014-06-13

4. Numerical Simulation of Excrescence Generated Transition;AIAA Journal;2014-02

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