Collapse mechanisms of sandwich beams with composite faces and a foam core, loaded in three-point bending. Part II: experimental investigation and numerical modelling

• Published in: International journal of mechanical sciences Vol. 46; no. 4; pp. 585 - 608
• Main Authors: Steeves, Craig A., Fleck, Norman A.
• Format: Journal Article
• Language: English
• Published: Elsevier Ltd 01.04.2004
• Subjects: Analytical solutions; Bending; Buckling failure; Composite materials; Indentation; Optimisation; Sandwich materials; Sandwich materials; Composite materials; Optimisation; Analytical solutions; Bending; Buckling failure; Indentation
• ISSN: 0020-7403; 1879-2162
• DOI: 10.1016/j.ijmecsci.2004.04.004

This study focuses on the competing collapse mechanisms for simply supported sandwich beams with composite faces and a PVC foam core subjected to three point bending. The faces comprise Hexcel Fibredux 7781-914G woven glass fibre-epoxy prepreg, while the core comprises closed cell Divinycell PVC foam of relative density 6.6% and 13.3%. The mechanical properties of the face sheets and core are measured independently. Depending upon the geometry of the beam and the relative properties of the constituents, collapse is by core shear, face sheet microbuckling or by indentation beneath the middle loading roller. A systematic series of experiments and finite element simulations have been performed in order to assess the accuracy of simple analytic expressions for the strength. In general, the analytic expressions for peak load are adequate; however, simple beam theory becomes inappropriate and the analytic models are inaccurate for stubby beams with thick faces relative to the core thickness. A failure mechanism map is constructed to reveal the dependence of the dominant collapse mechanism upon the geometry of the beam.