Lift-to-Drag Ratio Improvement of a Supersonic Transport with Leading-Edge and Trailing-Edge Flaps-Reference-Cited by-同舟云学术

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Lift-to-Drag Ratio Improvement of a Supersonic Transport with Leading-Edge and Trailing-Edge Flaps

Published:2003 Issue:597 Volume:51 Page:551-558
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Kwak Dong-Youn,Miyata Katsuhiro,Noguchi Masayoshi,Rinoie Kenichi

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/51/597/51_597_551/_pdf

Reference7 articles.

1. 2) Coe, P. L., Jr. and Weston, R. P.: Effects of Wing Leading-Edge Deflection on Low-Speed Aerodynamic Characteristics of a Low Aspect-Ratio Highly Swept Arrow-Wing Configuration, NASA TP-1434, 1979.

2. 3) Coe, P. L., Jr., Kjelgaard, S. O. and Gentry, G. L., Jr.: Low-Speed Aerodynamic Characteristics of a Highly Swept, Untwisted, Uncambered Arrow Wing, NASA TP-2176, 1983.

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. Static Roll Characteristics of an SST at High Angle of Attack;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2006

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