4.6 Article

Experimental and numerical study of low-velocity impact damage in sandwich panel with UHMWPE composite facings

Journal

Publisher

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ijsolstr.2023.112519

Keywords

Low velocity impact (LVI); Failure mechanisms; Sandwich composite panel (SCP); Computed micro-tomography ( mu CT); Ultra-high molecular weight polyethylene; (UHMWPE); Finite element modelling

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This paper investigates the low-velocity impact response and damage mechanisms of sandwich composite panels with UHMWPE composite facings and PVC/PET foam cores. Experimental tests and numerical simulations are conducted to analyze the effects of areal density and foam type on the impact characteristics of the panels. The results show that panels with PET foam cores exhibit higher impact strength and energy absorption performance, indicating the potential for optimizing the LVI resistance of SCPs.
This paper is concerned with the low-velocity impact (LVI) response behaviour of sandwich composite panels (SCPs) with ultra-high molecular weight polyethylene (UHMWPE) composite facings and Polyvinyl Chloride (PVC)/Polyethylene Terephthalate (PET) foam cores. A series of LVI tests with SCPs subjected to 50 J, 80 J and 110 J were conducted to examine their impact characteristics and damage mechanisms. LVI-induced internal damage in the SCPs were characterised by compute micro-tomography (mu CT) analysis. The effects of UHMWPE areal density and foam type on the LVI responses and associated failure modes of the panels were also examined. The experimental results showed that the SCP with a PET foam core exhibited higher impact strength and energy absorption performance than those of the panel with a PVC foam core. In addition, a finite element (FE) model incorporating the Puck's failure criteria, cohesive law and crushable foam plasticity model was developed and validated to predict the intra-and inter-laminar damages of SCPs. Finally, several failure mechanisms (fibre failure, matrix cracking and local delamination) of SCPs during LVI was thoroughly discussed. The results show the UH170-PET specimen has the best impact resistance and energy absorption performance. The parametric analysis of the areal density and foam type has revealed that these parameters can be optimised for the best LVI resistance of SCPs. These findings are helpful for designing lightweight foam-based sandwich composite structures with superior impact resistance.

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