Dynamic Characteristics of Rolling Delta Wing with High Angle of Attack under the Ground Effect-Reference-Cited by-同舟云学术

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Dynamic Characteristics of Rolling Delta Wing with High Angle of Attack under the Ground Effect

Published:2004 Issue:605 Volume:52 Page:272-279
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:

Kawazoe Hiromitsu,Morita Shinji

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/52/605/52_605_272/_pdf

Reference22 articles.

1. 1) Elle, B. J.: On the Breakdown at High Incidences of the Leading-Edge Vortices on Delta Wing, J. Roy. Aero. Soc., 64 (1960), p. 596.

2. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy

3. 3) Nguyen, L. T., Yip, L. and Chambers, J. R.: Self-Induces Wing Rock of Slender Delta Wings, AIAA Paper 81-1883, 1981.

4. The fluid mechanics of slender wing rock

5. Dynamic load measurements with delta wings undergoing self-induced roll oscillations

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