A Method of Inflatable Leading Edge for High Lift,Deicing and Noise Reduction-Reference-Cited by-同舟云学术

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A Method of Inflatable Leading Edge for High Lift,Deicing and Noise Reduction

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
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Author:

Jiang Yuewen¹,Ye Zhengyin¹,Zhang Zhengke¹

Affiliation:

1. National Key Laboratory of Aerodynamic Design and Research in Northwestern Polytechnical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-747

Reference21 articles.

1. Gurney flap—Lift enhancement, mechanisms and applications

2. 3Tinoco, E.N., Ball, D.N., and Rice, F.A. "Pan air analysis of a transport high lift configuration," AIAA Paper 86-1811.

3. Thin-Airfoil Theoretical Interpretation for Gurney Flap Lift Enhancement

4. 5Henne,P.A.,andGregg,R.D."Newairfoildesignconcept,"AIAAPaper89-2201.

Cited by 1 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. Novel Method Based on Inflatable Bump for Vertical Tail Buffeting Suppression;Journal of Aircraft;2015-01

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