Influence of multi-impacts on GFRP composites laminates

Abstract The behaviour of Glass Fibre Reinforced Composites (GFRPs) under single and multi-impact events of the same total energy was analysed. Experimental tests were performed considering circular simple supported plates impacted on its centre. The analyses of the results issuing from load–time, load–displacement and energy–time curves have shown that the sole impact of 3 J is more detrimental for the plate, relative to the other cases of cumulative damage (1 J + 2 J and 1 J + 1 J + 1 J). A fine-tune analysis of damage evolution between subsequent impacts using a numerical procedure including a cohesive mixed-mode damage model was also performed. This analysis permits to verify the evolution of the projected delaminated area as well as the fracture process zone in the vicinity of delaminations. It was verified that a negligible evolution of damage occurs in the case of three consecutive impacts of the same energy. Additionally, it was concluded that the cumulative damage in the case of (1 J + 2 J) is inferior to the one propitiated by the sole impact of maximum energy (3 J).

[1]  Hiroyuki Hamada,et al.  Fractography of fracture in CFRP under compressive load , 1997 .

[2]  S. Monteiro,et al.  Evaluation of repeated low energy impact damage in carbon–epoxy composite materials , 2005 .

[3]  S. Xu,et al.  Prediction of Low Velocity Impact Damage in carbon/epoxy Laminates☆ , 2013 .

[4]  M.F.S.F. de Moura,et al.  Modelling the interaction between matrix cracking and delamination in carbon–epoxy laminates under low velocity impact , 2004 .

[5]  G.A.O. Davies,et al.  Impact damage and residual strengths of woven fabric glass/polyester laminates , 1996 .

[6]  B. M. Icten Repeated impact behavior of glass/epoxy laminates , 2009 .

[7]  J. Ferreira,et al.  Impact response of Kevlar composites with nanoclay enhanced epoxy matrix , 2013 .

[8]  Peter Cawley,et al.  A review of defect types and nondestructive testing techniques for composites and bonded joints , 1988 .

[9]  J. Ferreira,et al.  Impact response of Kevlar composites with filled epoxy matrix , 2012 .

[10]  M. Richardson,et al.  Review of low-velocity impact properties of composite materials , 1996 .

[11]  M. D. de Moura,et al.  Residual Strength after Low Velocity Impact in Carbon-Epoxy Laminates , 2006 .

[12]  S. Abrate Impact on Laminated Composite Materials , 1991 .

[13]  M.F.S.F. de Moura,et al.  Prediction of low velocity impact damage in carbon–epoxy laminates , 2002 .

[14]  J. Lankford Shear versus dilatational damage mechanisms in the compressive failure of fibre-reinforced composites , 1997 .

[15]  A. Waas,et al.  Compressive splitting response of glass-fiber reinforced unidirectional composites , 2000 .

[16]  S. Monteiro,et al.  Effect of the laminate thickness on the composite strength to repeated low energy impacts , 2005 .

[17]  M. D. Moura,et al.  Damage detection on laminated composite materials using several NDT techniques , 2012 .

[18]  Shaik Jeelani,et al.  Studies on the low-velocity impact response of woven hybrid composites , 2005 .

[19]  António Torres Marques,et al.  Numerical simulation of the drilling process on carbon/epoxy composite laminates , 2006 .

[20]  K. Iqbal,et al.  Impact damage resistance of CFRP with nanoclay-filled epoxy matrix , 2009 .

[21]  S. Jeelani,et al.  Experimental investigations on the response of stitched/unstitched woven S2-glass/SC15 epoxy composites under single and repeated low velocity impact loading , 2003 .

[22]  M. D. de Moura,et al.  Delamination Effect on Bending Behaviour in Carbon–Epoxy Composites , 2011 .

[23]  T. Peijs,et al.  Compressive failure mechanisms in multi-fibre microcomposites , 2004 .

[24]  A. Mouritz,et al.  Flexural Strength and Interlaminar Shear Strength of Stitched GRP Laminates Following Repeated Impacts , 1997 .

[25]  F. V. Antunes,et al.  Effect of Interlayer Delamination on Mechanical Behavior of Carbon/Epoxy Laminates , 2009 .

[26]  J. Doong,et al.  Impact Fatigue of Short Glass Fiber Reinforced Polycarbonate , 1997 .

[27]  R. Zaera,et al.  Damage in CFRPs due to low velocity impact at low temperature , 2005 .

[28]  D. Adams,et al.  Damage sustained by a carbon/ epoxy composite material subjected to repeated impact , 1988 .