Abstract

Sandwich composites are of interest in marine applications due to their high strength-to-weight ratio and tailorable mechanical properties, but their resistance to air blast loading is not well understood. Full-scale 100 kg TNT equivalent air blast testing at a 15 m stand-off distance was performed on glass-fibre reinforced polymer (GFRP) sandwich panels with polyvinyl chloride (PVC); polymethacrylimid (PMI); and styrene acrylonitrile (SAN) foam cores, all possessing the same thickness and density. Further testing was performed to assess the blast resistance of a sandwich panel containing a stepwise graded density SAN foam core, increasing in density away from the blast facing side. Finally a sandwich panel containing compliant polypropylene (PP) fibres within the GFRP front face-sheet, was subjected to blast loading with the intention of preventing front face-sheet cracking during blast. Measurements of the sandwich panel responses were made using high-speed digital image correlation (DIC), and post-blast damage was assessed by sectioning the sandwich panels and mapping the damage observed. It was concluded that all cores are effective in improving blast tolerance and that the SAN core was the most blast tolerant out of the three foam polymer types, with the DIC results showing a lower deflection measured during blast, and post-blast visual inspections showing less damage suffered. By grading the density of the core it was found that through thickness crack propagation was mitigated, as well as damage in the higher density foam layers, thus resulting in a smoother back face-sheet deflection profile. By incorporating compliant PP fibres into the front face-sheet, cracking was prevented in the GFRP, despite damage being present in the core and the interfaces between the core and face-sheets.

Highlights

  • The high strength-to-weight ratio and tailorable mechanical properties of polymeric sandwich composites makes them attractive for marine applications

  • This area of research is still not fully understood and the research presented in this paper considers the effect on panel response of three different foam core polymer types for use in sandwich composites: polyvinyl chloride (PVC); polymethacrylimid (PMI); and styrene acrilonitrile (SAN)

  • The digital image correlation (DIC) responses of the single layer styrene acrylonitrile (SAN) foam core sandwich panel are shown in Fig. 7(a) illustrates the contour plots of the out of plane displacement (UZ) and the maximum principal strain, where discontinuties in displacement, and early concentrated strains are visible along the vertical edges of the panel, indicating core cracking

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Summary

Introduction

The high strength-to-weight ratio and tailorable mechanical properties of polymeric sandwich composites makes them attractive for marine applications. In some scenarios it is important that these materials are tested under blast loading conditions This area of research is still not fully understood and the research presented in this paper considers the effect on panel response of three different foam core polymer types for use in sandwich composites: polyvinyl chloride (PVC); polymethacrylimid (PMI); and styrene acrilonitrile (SAN). Arora et al [1] performed full-scale air blast testing on glass fibre reinforced polymer (GFRP) skin sandwich composites with 40 mm thick styrene acrylonitrile (SAN) foam cores, implementing 30 kg Composition 4 (C4) plastic explosive The response of these test panels was measured using digital image correlation (DIC). Arora et al [2] performed further full-scale air blast research considering the effect of sandwich core thickness on panel response, and performed underwater blast testing on polymeric foam sandwich panels and GFRP tubular structures. The responses of all of these test panels were measured using DIC, and the post-blast damage was assessed by sectioning the blast panels to visually inspect the defects

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