Experimental and Numerical Studies of Geometry Effects on UCAV's Aerodynamics-Reference-Cited by-同舟云学术

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Experimental and Numerical Studies of Geometry Effects on UCAV's Aerodynamics

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Huang Xing¹,Mébarki Youssef²,Benmeddour Ali²,Brown Todd²

Affiliation:

1. National Research Council

2. IAR/NRC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-403

Reference10 articles.

1. Numerical simulation of forced and free-to-roll delta-wing motions

Cited by 5 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. Leading-Edge Radius Effects on Aerodynamic Characteristics of 50-Degree Delta Wings;Journal of Aircraft;2012-03

2. Key Parameters and Conceptual Configuration of Unmanned Combat Aerial Vehicle Concept;Chinese Journal of Aeronautics;2009-08

3. Leading-Edge Radius Effects on 50-deg Delta Wing Flow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

4. Effects of Leading-Edge Shape on the Flow Over 50-deg Delta Wings;26th AIAA Applied Aerodynamics Conference;2008-06-14

5. Unsteady aerodynamics of nonslender delta wings;Progress in Aerospace Sciences;2005-10

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