Optimal design of tube flexure cut-out geometries for viscoelastic resilience and deployment performance

被引:0
|
作者
Kunakorn-ong, Pathawee [1 ]
Santer, Matthew [1 ]
机构
[1] Imperial Coll London, Dept Aeronaut, London SW7 2AZ, England
关键词
Tube flexure; Viscoelasticity; Deployable structure; Bayesian optimization; COMPOSITE; ONBOARD;
D O I
10.1016/j.actaastro.2024.01.012
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a methodology for the design of deployable tube flexures made of ultra-thin carbon fiber composite. The proposed process aims to enhance viscoelastic resilience on recovery time after longterm stowage through the design of cut -out geometries. Viscoelasticity is modeled using an experimentally determined Prony series master curve. Bayesian optimization is employed to determine cut -out shapes based on the recovery time and Hashin failure criteria. Partial dependent plots are implemented to interpret the effect of cut -out formation on deployment performance. These reveal optimal profiles of cut -out shapes to achieve a desired operational performance. The efficiency of the proposed methodology is validated by experiment.
引用
收藏
页码:282 / 294
页数:13
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