Abstract
This paper develops a tri-stable structure that consists of four bi-stable rectangular laminates. The tri-stable structure can exhibit three different stable geometric configurations: plane, concave, and convex configurations. The structure can also be snapped between the various states. The design and fabrication methods of the tri-stable structure using bi-stable rectangular laminates are presented. A two-step finite element simulation is performed to predict the critical load to snap the tri-stable structure and to capture the snap-through process. The predicted curvatures and the critical loads from the finite element analysis show a high agreement with the experimental results. The tri-stable structures and the proposed two-step method should be instructive to design and construct the multi-stable structures and to understand their snap-through process.
| Original language | English |
|---|---|
| Pages (from-to) | 1497-1504 |
| Number of pages | 8 |
| Journal | Composites Part A: Applied Science and Manufacturing |
| Volume | 43 |
| Issue number | 9 |
| DOIs | |
| State | Published - Sep 2012 |
Keywords
- A. Lamina/ply
- B. Buckling
- C. Finite element analysis (FEA)
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