Abstract
![CDATA[In-plane dynamic crushing and energy-absorption capabilities of chiral honeycombs are studied numerically invoking Finite Element (FE) code ABAQUS®/Explicit. Chiral honeycombs are characterized by a non-intuitive negative in-plane Poisson’s ratio ρ (auxeticity), for hexagonal chiral honeycombs, which exhibits a theoretic value of −1 (Prall and Lakes, 1997). The effects of topology parameters, stiffness ratio of ligament to node, impact velocity and impact mass on structural crashworthiness are studied based on a fixed-size model and a convergence study is also carried out to minimize the meshing induced result error. The numerical results show that increasing values of topology parameters give rise to better crashworthiness of chiral honeycombs which is dependent on boundary conditions. Specific energy absorption of chiral honeycomb is independent of relative stiffness after reaching a critical value. High velocity impact loading has dramatic effect on energy absorption of chiral honeycomb which is relatively independent of low velocity impact loading and impact mass.]]
Original language | English |
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Title of host publication | Mechanics of Structures and Materials: Advancements and Challenges: Proceedings of the 24th Australasian Conference on the Mechanics of Structures and Materials (ACMSM24), Perth, Australia, 6-9 December 2016 |
Publisher | CRC Press |
Pages | 889-894 |
Number of pages | 6 |
ISBN (Print) | 9781138029934 |
Publication status | Published - 2017 |
Event | Australasian Conference on the Mechanics of Structures and Materials - Duration: 6 Dec 2016 → … |
Conference
Conference | Australasian Conference on the Mechanics of Structures and Materials |
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Period | 6/12/16 → … |
Keywords
- airplanes
- crashworthiness
- finite element method
- honeycomb structures
- topology