Published August 2019 | Version v1
Journal article

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.