Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number-Reference-Cited by-同舟云学术

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Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:6th AIAA Flow Control Conference
language:
Short-container-title:

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/10.2514/6.2012-2956

Reference73 articles.

1. AIAA Education Series;Mueller T. J.,2007

2. 3Wadlin, K. L., Ramsen, J. A., and Vaughn, V. L. “The Hydrodnamic Characteristics of Modified Rectangular Flat Plates Having Aspect Ratios of 1.00, 0.25, and 0.125 and Operating Near a Free Water Surface,” NACA Technical Report 1246, National Advisory Committee for Aeronautics, 1955.

3. Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds

4. Vortex-lift prediction for complex wing planforms.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Suction control of flow separation of a low-aspect-ratio wing at a low Reynolds number;Fluid Dynamics Research;2018-09-24

2. Investigation of an Improved Design for a Dielectric Barrier Discharge Plasma Actuator for Flight Control of an Inflatable Wing;52nd Aerospace Sciences Meeting;2014-01-10

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