Prediction of failure modes and peak loads in lattice sandwich panels under three-point loading
Source abstract
Abstract
In this study, the failure behaviour of lattice sandwich panels under three-point loading has been studied using a nonlinear finite element analysis. The failure mechanisms of lattice-cored sandwich panels can be classified in three modes; facesheet yielding, facesheet wrinkling and core shear. When the panel fails due to facesheet yielding or core shear, the evaluation of the strength of the lattice-cored panel can be undertaken in the same manner as that of a foam-cored panel. In contrast, when wrinkle-like deformation occurs in the facesheets, the failure load can be estimated from the buckling stress of the facesheet. The failure mode map for the lattice-cored panel with the coordinate system t f / l and [Formula: see text] can be described by the analytical equations that predict the three failure modes. The failure mode map highlights the dominant failure modes for the lattice-cored sandwich panel based on the key design parameters t f / l and [Formula: see text].
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Research context
OpenAlex topics: Cellular and Composite Structures · Polymer composites and self-healing · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Graduate School of Mechanical Engineering, Tokyo University of Science, Tokyo, Japan
Faculty of Engineering, Tokyo University of Science, Tokyo, Japan
National Center for International Research on Structural Health Management of Critical Components, Jiangsu University, Zhenjiang, China
Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi, UAE
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