Abstract
The high velocity impact response of a range of polypropylene-based fibre-metal laminate (FML) structures has been investigated. Initial tests were conducted on simple FML sandwich structures based on 2024-O and 2024-T3 aluminium alloy skins and a Self-Reinforced Polypropylene (SRPP) composite core. Here, it was shown that laminates based on the stronger 2024-T3 alloy offered a superior perforation resistance to those based on the 2024-O system. Tests were also conducted on multi-layered materials in which the composite plies were dispersed between more than two aluminium sheets. For a given target thickness, the multi-layered laminates offered a superior perforation resistance to the sandwich laminates. The perforation resistances of the various laminates investigated here were compared by determining the specific perforation energy (s.p.e) of each system. Here, the sandwich FMLs based on the low density SRPP core out-performed the multi-layer systems, offering s.p.e.’s roughly double that exhibited by a similar Kevlar-based laminate. A closer examination of the panels highlighted a number of failure mechanisms such as ductile tearing, delamination and fibre failure in the composite plies as well as permanent plastic deformation, thinning and shear fracture in the metal layers. Finally, the perforation threshold of all of the FML structures was predicted using the Reid–Wen perforation model. Here, it was found that the predictions offered by this simple model were in good agreement with the experimental data.
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References
Peters, S.T. (ed.): Handbook of Composites. Chapman & Hall, London (1998)
Matthews, F.L., Rawlings, R.D.: Composites Structures and Materials. CRC Press, Boca Raton (FL) (1999)
Kelly, A. (ed.):Concise Encyclopaedia of Composite Materials (revised). Elsevier, Amsterdam (1994)
Prichard, J.C., Hogg, P.J.:The Role of Impact Damage in Post-impact Compression Testing. Composites 21, 503–511 (1990)
Dorey, G., Bishop, S.M., Curtis, P.T.: On he impact performance of carbon–fibre laminates with epoxy and PEEK matrices. Compos. Sci. Technol. 23, 221–237 (1985)
Zhou, G.: Prediction of Impact amage thresholds of glass-fiber-reinforced laminates. Compos. Struct. 31, 185–193 (1995)
Cantwell, W.J., Curtis, P., Morton, J.: An assessment of the impact performance of CFRP reinforced with high strain carbon fibres. Compos. Sci. Technol. 25, 133–148 (1986)
Thanomsilp, C., Hogg, P.J.: Penetration impact resistance of hybrid composites based on commingled yarn fabrics. Compost. Sci. Technol. 63, 467–482 (2003)
Abrate, S.: Impact on laminated composite materials. Appl. Mech. Rev. 44, 155–190 (1991)
Dorey, G., Sidey, S.G.R., Hutchings, J.: Properties of carbon fiber-Kevlar 49 fiber hybrid composites. Composites 9, 25–32 (1978)
Krishnakumar, S.: The synthesis of metals and composites. Mater. Manuf. Process. 9, 295–354 (1994)
Alderliesten, R.C.: Fatigure. In: Vlot, A., Gunnick. J.W. (eds).: Fibre–metal laminates: an introduction [Chap. 11]. Kluwer, Dordrecht (2001)
Reyes-Villanueva, G.: PhD thesis, University of Liverpool (2002)
Vlot, A.D., Kroon, E., La Rocca, G.: Impact response of fiber metal laminates. Key. Eng. Mater. 141–143, 235–276 (1998)
Reyes-Villanueva, G., Cantwell, W.J.: The mechanical properties of fibre–metal laminates based on glass fibre reinforced Polypropylene. Compos. Sci. Technol. 60, 1085–1094 (2000)
Cantwell, W.J., Wade, G., Guillen, G.F., Reyes-Villanueva, G., Jones, N., Compston, P.: The high velocity impact response of novel fiber–metal laminates. In: Proceedings of the ASME conference, New York (2001)
Reid, S.R., Wen. H.M.: Perforation of FRP laminates and sandwich panels subjected to missile impact. In: Reid, S.R., Zhou, G., (eds.): Impact behaviour of fibre-reinforced composite materials and structures, pp. 239–279. Woodhead, Cambridge (2000)
Morye, S.S., Hine, P.J., Duckett, R.A., Carr, D.J., Ward, I.M.: Modelling of the energy absorption by polymer composites upon ballistic impact. Compos. Sci. Technol. 60, 2631–2642 (2000)
Sun, C.T., Potti, S.V.: High velocity impact and penetration of composite laminates. In: Miravete, V.A., (ed.): ICCM/9 Composite Behaviour, pp. 261–68. Woodhead, Cambridge (1993)
Bland, P.W., Dear. J.P.: Observation on the impact behaviour of carbon-fibre reinforced polymers for the qualitative validation of models. Composites: Part A . 32, 1217–1227 (2001)
Available from: www.curvonline.com
Hagenbeek, M.: Impact properties. In: Vlot, A., Gunnick, J.W., (eds.): Fibre–metal laminates: an introduction [Chap. 27]. Kluwer, Dordrecht (2001)
Shockey, D.A., Erlich, D.C., Simmons, J.W.: Full-scale tests of lightweight fragment barriers on commercial aircraft, final report DOT/FAA/AR-99/71 (1999)
Acknowledgments
The authors acknowledge the financial support of the Public Service Department (Malaysia) and Universiti Teknologi Malaysia. The authors are also grateful to Derek Riley of Propex Fabric for supplying the self-reinforced composite (Curv) and David Robinson and Professor Tony Johnson of Gluco Ltd., Leeds, UK for supplying the interlayer adhesive (Gluco), and to Mr. Peter Smith for his help in conducting the impact tests.
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Abdullah, M.R., Cantwell, W.J. (2012). The High Velocity Impact Response of Self-Reinforced Polypropylene Fibre Metal Laminates. In: Tamin, M. (eds) Damage and Fracture of Composite Materials and Structures. Advanced Structured Materials, vol 17. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-23659-4_13
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DOI: https://doi.org/10.1007/978-3-642-23659-4_13
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