折叠(DSP实现)
圆柱
波纹管
过程(计算)
压力(语言学)
数学
材料科学
几何学
结构工程
计算机科学
工程类
机械工程
语言学
操作系统
哲学
作者
Jae Mi Suh,Tae Hyun Kim,Jae-Hung Han
出处
期刊:Journal of Spacecraft and Rockets
[American Institute of Aeronautics and Astronautics]
日期:2021-03-01
卷期号:58 (2): 516-530
被引量:12
摘要
A new approach for folding the Yoshimura cylinder is proposed in this study. The proposed concept is based on a reconfiguration process involving a cylindrical structure with the Yoshimura pattern and the bellows fold pattern. Static analyses are conducted to confirm the effectiveness of the proposed folding methodology. A special case of folding is observed that does not create wrinkles in the fully folded state. A mathematical problem is established and three governing equations are derived from the problem. The special folding pattern is determined by solving the three governing equations. The most geometrically and structurally efficient configuration for the reconfigured cylinder is determined. A geometrical analysis is conducted for various configurations of the cylinder that can be observed in the proposed folding methodology. The proposed folding methodology folds the Yoshimura cylinder much more efficiently in terms of required force and stress compared to the conventional folding approach.
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