High strain rate response of S2-glass/epoxy composites with polycarbonate facing

Citation
Uk. Vaidya et al., High strain rate response of S2-glass/epoxy composites with polycarbonate facing, POLYM POL C, 9(2), 2001, pp. 67-80
Citations number
15
Categorie Soggetti
Material Science & Engineering
Journal title
POLYMERS & POLYMER COMPOSITES
ISSN journal
09673911 → ACNP
Volume
9
Issue
2
Year of publication
2001
Pages
67 - 80
Database
ISI
SICI code
0967-3911(2001)9:2<67:HSRROS>2.0.ZU;2-C
Abstract
Impact damage is of critical concern in structures using laminated fibre re inforced composites. Thermoplastic polycarbonate (PC) offers high impact re sistance and is often used in a variety of applications, including the wind shield and canopy of aircraft, pressure windows and automotive parts among others. Impact damage to structures utilizing composites has been an area o f constant concern. In the current study, S2-glass/epoxy composite laminate s bonded to PC (referred to as 'S2-glass/epoxy-PC' or 'Laminate-PC') have b een investigated for their high strain rate (HSR) impact response. A compre ssion Split Hopkinson Pressure Bar (SHPB) with 19.05 mm (0.75") incident an d transmission bars with dynamic recovery technique was used to test four, six and eight layers S2-glass/epoxy-PC samples. Using dynamic recovery tech nique on the SHPB, the sample was subjected to a controlled single compress ive pulse, providing information on damage evolution. The samples were test ed under HSR impact in three directions (with respect to the side facing th e incident bar of the SHPB). In the first, the PC faced the incident bar, i n the second, the S2-glass/epoxy laminate faced the same, whereas in the th ird, the loading was in the in-plane direction of the laminate. The HSR imp act tests were performed by considering three strain rates - 109, 327 and 5 44/s - for all the experiments. The results of the investigation showed tha t providing a PC facing to S2-glass/epoxy laminate is an effective way of o btaining deformation in the PC facing which absorbs a large portion of the incident energy, thereby minimizing any delamination threat to the composit e backing. PC acts as a sacrificial layer that can be readily replaced in t he application.