A Computational Fluid Dynamics Investigation of the 1303 UCAV Configuration with Deployable Rao Vortex Flaps-Reference-Cited by-同舟云学术

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A Computational Fluid Dynamics Investigation of the 1303 UCAV Configuration with Deployable Rao Vortex Flaps

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Atkinson Michael¹,Ferguson Frederick¹

Affiliation:

1. Center for Aerospace Research, North Carolina A&T State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1262

Reference18 articles.

1. Ghee, T.A. "Parametric Evaluation of Deployable Serrated Flaps on a Representative UCAV Configuration." AIAA-2003-3928

2. Ghee, T.A. "A Deployable Serrated Flap for Air Vehicle Control of a Representative UCAV Configuration" AIAA-2002-3276.

Cited by 3 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. Design of Vortex Flaps for Reducing Approach Speed of a Supersonic Naval Fighter Aircraft;Lecture Notes in Mechanical Engineering;2020

2. Aerodynamics of UAV Configurations;Advanced UAV Aerodynamics, Flight Stability and Control;2017-05-05

3. Conformal s-Shaped Inlet Design and Flow Field Characteristics of Flying Wing Unmanned Aerial Vehicle;Advanced Materials Research;2014-06

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