Flutter and discrete gust load alleviation characteristics of multi-segment folding wings with constant cross section
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics
Reference27 articles.
1. Continuum aeroelastic model for a folding-wing configuration;Liska;AIAA J.,2009
2. Nonlinear aeroelastic study for folding wing structures;Attar;AIAA J.,2010
3. Aeroelastic study for folding wing during the morphing process;Hu;J. Sound Vib.,2016
4. Nonlinear folding wing tips for gust loads alleviation;Castrichini;J. Aircr.,2016
5. Nonlinear negative stiffness wingtip spring device for gust loads alleviation;Castrichini;J. Aircr.,2017
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. Flutter Characteristics of a Modified Z-Shaped Folding Wing Using a New Non-Intrusive Model;Aerospace;2024-05-24
2. Model Order Reduction and Nonlinear Dynamic Analysis of the Folding Fin with Freeplay Nonlinearity;Journal of Vibration Engineering & Technologies;2024-04-30
3. Approximate global mode method for flutter analysis of folding wings;International Journal of Mechanical Sciences;2024-03
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