TY - GEN
T1 - Damage characterization of E-glass and C-glass fibre polymer composites after high velocity impact
AU - Razali, N.
AU - Sultan, M. T.H.
AU - Cardona, F.
AU - Jawaid, M.
N1 - Publisher Copyright:
© 2017 Author(s).
PY - 2017/12/4
Y1 - 2017/12/4
N2 - The purpose of this work is to identify impact damage on glass fibre reinforced polymer composite structures after high velocity impact. In this research, Type C-glass (600 g/m2) and Type E-glass (600 g/m2) were used to fabricate Glass Fibre-Reinforced Polymer composites (GFRP) plates. The panels were fabricated using a vacuum bagging and hot bounder method. Single stage gas gun (SSGG) was used to do the testing and data acquisition system was used to collect the damage data. Different types of bullets and different pressure levels were used for the experiment. The obtained results showed that the C-glass type of GFRP experienced more damage in comparison to E-glass type of materials based on the amount of energy absorbed on impact and the size of the damage area. All specimens underwent a partial fibre breakage but the laminates were not fully penetrated by the bullets. This indicated that both types of materials have high impact resistance even though the applied pressures of the gas gun were on the high range. We concluded that within the material specifications of the laminates including the type of glass fibre reinforcement and the thickness of the panels, those composite materials are safe to be applied in structural and body armour applications as an alternative to more expensive materials such as Kevlar and type S-glass fibre based panels.
AB - The purpose of this work is to identify impact damage on glass fibre reinforced polymer composite structures after high velocity impact. In this research, Type C-glass (600 g/m2) and Type E-glass (600 g/m2) were used to fabricate Glass Fibre-Reinforced Polymer composites (GFRP) plates. The panels were fabricated using a vacuum bagging and hot bounder method. Single stage gas gun (SSGG) was used to do the testing and data acquisition system was used to collect the damage data. Different types of bullets and different pressure levels were used for the experiment. The obtained results showed that the C-glass type of GFRP experienced more damage in comparison to E-glass type of materials based on the amount of energy absorbed on impact and the size of the damage area. All specimens underwent a partial fibre breakage but the laminates were not fully penetrated by the bullets. This indicated that both types of materials have high impact resistance even though the applied pressures of the gas gun were on the high range. We concluded that within the material specifications of the laminates including the type of glass fibre reinforcement and the thickness of the panels, those composite materials are safe to be applied in structural and body armour applications as an alternative to more expensive materials such as Kevlar and type S-glass fibre based panels.
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U2 - 10.1063/1.5010568
DO - 10.1063/1.5010568
M3 - Conference contribution
AN - SCOPUS:85038380703
T3 - AIP Conference Proceedings
BT - Advanced Materials for Sustainability and Growth
A2 - Ibrahim, Suhaina Mohd
A2 - Noorsal, Kartini
A2 - Ibrahim, Suhaina Mohd
PB - American Institute of Physics Inc.
T2 - 3rd Advanced Materials Conference 2016, AMC 2016
Y2 - 28 November 2016 through 29 November 2016
ER -