The structure response of sandwich beams with metallic auxetic honeycomb cores under localized impulsive loading-experiments and finite element analysis
- 1. Beijing Key Laboratory of Lightweight Multi-functional Composite Materials and Structures, Institute of Advanced Structure Technology, Beijing Institute of Technology, Beijing 100081 (China)
- 2. Departments of Naval Architecture, Ocean and Structural Engineering, School of Transportation, Wuhan University of Technology, Wuhan 430063 (China)
- 3. Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, MA 02139 (United States)
- 4. State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081 (China)
Description
Highlights: • The structure response of sandwich beam with reentrant honeycomb core under locally impact was firstly studied. • The local negative Poisson's ratio deformation was observed in the reentrant honeycomb core. • The relationship between residual deflection of sandwich beam with reentrant honeycomb core and local impulse was linear. -- Abstract: In recent years, auxetic cellular materials such as auxetic reentrant honeycombs were widely studied due to its attractively negative Poisson's ratio. In this manuscript, the structure response of end-clamped sandwich beam with auxetic reentrant hexagonal aluminum honeycomb core locally subjected to foam projectile with high-velocity impact was experimentally and numerically studied. The reentrant honeycomb cores with different cell-wall thicknesses were fabricated by selective laser melting (SLM). According to experiment results, the failure modes of the sandwich beam were investigated. It was found that sandwich beam with different honeycomb cell's thicknesses could fail in different modes. Meanwhile, the local negative Poisson's ratio deformation was observed in the thin honeycomb core. Based on this, a finite element (FE) model was constructed to analysis the dynamic deformation evolution of two face sheets and auxetic reentrant honeycomb core. The local auxetic and expand deformations of honeycomb core were both found. Finally, the residual deflections of sandwich beam under impulsive loadings were discussed.
Additional details
Identifiers
- DOI
- 10.1016/j.matdes.2019.107840;
- PII
- S0264127519302783;
Publishing Information
- Journal Title
- Materials and Design
- Journal Volume
- 176
- Journal Page Range
- vp.
- ISSN
- 0264-1275
- CODEN
- MADSD2
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 55050300
- Subject category
- S36: MATERIALS SCIENCE;
- Descriptors DEI
- 3D PRINTING; ALUMINIUM; CELL WALL; DEFORMATION; FINITE ELEMENT METHOD; PULSES; SCANNING LIGHT MICROSCOPY; THICKNESS
- Descriptors DEC
- CALCULATION METHODS; CELL CONSTITUENTS; COMPUTER-AIDED FABRICATION; DIMENSIONS; ELEMENTS; FABRICATION; MATHEMATICAL SOLUTIONS; METALS; MICROSCOPY; NUMERICAL SOLUTION; OPTICAL MICROSCOPY
Optional Information
- Copyright
- Copyright (c) 2019 The Authors. Published by Elsevier Ltd.