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Numerical modelling of honeycomb core crush behaviour
Authors:Levent Aktay,Bernd-H. Krö  plin
Affiliation:a Institute of Structures and Design, German Aerospace Center (DLR), Stuttgart, Germany
b Institute for Statics and Dynamics of Aerospace Structures (ISD), University of Stuttgart, Stuttgart, Germany
Abstract:In this work several numerical techniques for modelling the transverse crush behaviour of honeycomb core materials were developed and compared with test data on aluminium and Nomex™ honeycomb. The methods included a detailed honeycomb micromechanics model, a homogenised material model suitable for use in FE code solid elements, and a homogenised discrete/finite element model used in a semi-adaptive numerical coupling (SAC) technique. The micromechanics model is shown to be suitable for honeycomb design, since it may be used to compute crush energy absorption for different honeycomb cell sizes, cell wall thicknesses and cell materials. However, the very fine meshes required make it unsuitable for analysis of large sandwich structures. The homogenised FE model may be used for such structures, but gives poor agreement when failure is due to core crushing. The SAC model is shown to be most appropriate for use in structural simulations with extensive compression core crushing failures, since the discrete particles are able to model the material compaction during local crushing.
Keywords:Honeycomb materials   Crushing   Micromechanical modelling   Semi-adaptive coupling technique
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