Comparison of the passive and active control gust alleviation of a flying‐wing aircraft-Reference-Cited by-同舟云学术

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Comparison of the passive and active control gust alleviation of a flying‐wing aircraft

Published:2018-12-13 Issue:13 Volume:2019 Page:421-423
ISSN:2051-3305
Container-title:The Journal of Engineering
language:en
Short-container-title:J. eng.

Author:

Liu Ying¹

Affiliation:

1. Flight Test CenterAVIC General Huanan Aircraft Industry Co. LtdZhuhaiPeople's Republic of China

Publisher

Institution of Engineering and Technology (IET)

Subject

General Engineering,Energy Engineering and Power Technology,Software

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/joe.2018.9016

Reference9 articles.

1. NollT.E. BrownJ.M. Perez‐DavisM.E.et al.: ‘Investigation of the Helios prototype aircraft mishap’ NASA Report 2004 vol. 1

2. Optimum stacking sequence design of composite materials part I: constant stiffness design;Ghiasi H.;Compos. Struct.,2009

3. Optimum stacking sequence design of composite materials part II: variable stiffness design;Ghiasi H.;Compos. Struct.,2010

4. Ply angle optimization of nonuniform composite beams subject to aeroelastic constraints;Evrard T.;AIAA J.,2000

5. Optimization of ply angles in laminated composite structures by a hybrid, asynchronous, parallel evolutionary algorithm;Keller D.;Compos. Struct.,2010

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. An efficient reduced-order framework for active/passive hybrid flutter suppression;The Aeronautical Journal;2022-05-02

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