Delamination Resistance of Laminates with Various Stacking Sequences against Low Velocity Impacts

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Abstract:

Effects of low-velocity-low-energy impacts on interlaminar damage extent in Glass/Epoxy laminate panels of [0°/90°]10, [0°10/90°10], [0°5/90°5]2, [0°5/-45°5/90°5/+45°5] layups were experimentally investigated. The tests were carried out at room temperature with the help of INSTRON CEAST9350 impact system. The initial impact energy was 18J, impactor mass equaled 4kg and the corresponding contact speed was 3 m/s. During the impacts panels were simply supported with a circular steel rings of inner diameters d=80mm. It was found that the amounts of dissipated energy substantially varied depending on the reinforcement sequence and that the lowest amount of energy was dissipated by the laminate panel of [0°/90°]10 reinforcement stacking sequence while the highest one by the panel of [0°10/90°10] reinforcement stacking sequence. Such results suggested that clustering reinforcement layers of the same reinforcement orientation produced negative effects with the regard to the resistance of laminates against impact induced damage.

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Solid State Phenomena (Volume 240)

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143-148

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August 2015

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© 2016 Trans Tech Publications Ltd. All Rights Reserved

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[1] C. Akin, M. Senel, An experimental study of low velocity impactresponse for composite laminated plates, J. van der Geer, J.A.J. Hanraads, R.A. Lupton, The art of writing a scientific article, Sayi 21, Nisan (2010) 77-90.

Google Scholar

[2] F. Mili, B. Necib, The effect of stacking sequence on the impact-induced damage in cross-ply E-glass/epoxy composite plates, Arch. Appl. Mech. 79 (2009) 1019-1031.

DOI: 10.1007/s00419-008-0272-z

Google Scholar

[3] N. Hongkarnjanakul1, C. Bouvet, S. Rivallant, The effect of stacking sequence on low-velocity impact response of composite laminatres ECCM15 Venice, Italy, (2012).

Google Scholar

[4] M.A. Will, T. Franz, G.N. Nuric, The effect of laminate stacking sequence of CFRP filament wound tubes subjected to projectile impact, Composite structures 58 (2002) 259-270.

DOI: 10.1016/s0263-8223(02)00050-8

Google Scholar

[5] K. -H. IM, N. -S. PARK, Y. -N. KIM, I. -Y. YANG, A study on impact characteristics of the stacking sequences in CFRP composites subjected to falling weight impact loading, International Journal of Automotive Technology, Vol. 4, No. 4, (2003).

Google Scholar

[6] S.A. Hitchen, R. Kemp, The effect of stacking sequence on impact damage in carbon fibre/epoxy composite, Composites 26 (1995) 207-214.

DOI: 10.1016/0010-4361(95)91384-h

Google Scholar

[7] C. Nageswaran, C. R. Bird, R. Takahashi, Phased array scanning of artificial and impact damage in carbon fibre reinforced plastic (CFRP), Insight Vol 48 (2006) 155-159.

DOI: 10.1784/insi.2006.48.3.155

Google Scholar

[8] E1441-97 Standard Guide for Computed Thomography (CT) Imaging.

Google Scholar