桁架
结构工程
翼
阻尼器
还原(数学)
工程类
支撑
航程(航空)
控制理论(社会学)
计算机科学
撑杆
航空航天工程
数学
几何学
人工智能
控制(管理)
作者
Christopher Patrick Szczyglowski,Simon A Neild,Branislav Titurus,Jason Zheng Jiang,Etienne Coetzee
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2019-11-01
卷期号:56 (6): 2260-2271
被引量:5
摘要
This paper presents a novel method for gust loads alleviation in a truss-braced wing in which an inerter-based device located in the truss-structure is used to reduce peak-loads during a discrete “1-cosine” gust. Three candidate layouts are considered, and the device parameters are optimized to target the response of the first three structural modes. It is demonstrated that either a single damper or a combination of inerter-based devices can be used to achieve a reduction of approximately 4% for spanwise locations inboard of the strut attachment point and that this reduction is consistent across the full range of gust gradients. Furthermore, it is noted that the inerter-based device has a significantly smaller damping coefficient than the case where just a damper is used and that the device parameter values are viable within the scope of an aerospace application.
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