Wind tunnel test and analysis on gust load alleviation of a transport-type wing-Reference-Cited by-同舟云学术

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Wind tunnel test and analysis on gust load alleviation of a transport-type wing

Published:1987-04-06 Issue: Volume: Page:
ISSN:
Container-title:28th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

MATSUZAKI Y.¹,UEDA T.²,MIYAZAWA T.²,MATSUSHITA H.²

Affiliation:

1. Nagoya University, Japan

2. National Aerospace Laboratory, Chofu, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-781

Reference24 articles.

1. Miyazawa, Y."Active Control for Aeroelastic Systems ( i n Japanese)," Ph.D. Dissertation,University of Tokyo, 1981.

2. A finite state aerodynamic model for a lifting surface in incompressible flow

3. Matsushita, H. "Study on Aerodynamic Transfer Function and its Application t o F l u t t e r Suppression ( i n Japanese)," Ph.D. Dissertation,University of Tokyo, 1982.

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. Development of an Active Wingtip for Aeroelastic Control;Aerospace;2023-08-04

2. Study on gust alleviation control and wind tunnel test;Science China Technological Sciences;2013-01-18

3. Approach to modeling and estimation for uncertain systems;Journal of Guidance, Control, and Dynamics;1989-09

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