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Composite Materials Research Progress

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254<br />

Maria Pia Cavatorta and Davide Salvatore Paolino<br />

energies up to a few impacts before perforation, when data show a rapid increase. Therefore,<br />

by looking at the DuI values in the first impacts, no prediction can be made as to whether or<br />

not laminate perforation will occur within test duration. In case of repeated impacts, DD data<br />

can monitor the efficiency of energy absorption impact after impact. Results show that DD<br />

values at the first impact are about the same, regardless of the impact energy. Moreover,<br />

regardless of the final output of the test (no perforation/perforation), DD values show an<br />

initial slight decrease followed by a rather constant phase. When perforation is to be achieved,<br />

DD values start to increase a few impacts before final failure.<br />

Acknowledgments<br />

The Authors wish to acknowledge valuable discussions with professor Giovanni Belingardi.<br />

References<br />

[1] Roy, R; Sarkar BK; Bose NR. Impact fatigue of glass fibre-vinylester resin composites.<br />

<strong>Composite</strong>s Part A, 2001, 32, 871-876.<br />

[2] Zhou, G. Static behaviour and damage of thick composite laminates. <strong>Composite</strong><br />

Structures, 1996, 36, 13-22.<br />

[3] Zhou, G; Davies, GAO. Impact response of thick reinforced polyester laminates.<br />

International Journal of Impact Engineering, 1995, 3, 357-374.<br />

[4] Sutherland, LS; Guedes Soares, C. Effects of laminate thickness and reinforcement type<br />

on the impact behaviour of E-glass/polyester laminates. <strong>Composite</strong>s Science and<br />

Technology, 1999, 59, 2243-2260.<br />

[5] Azouaoui, K; Rechak, S; Azari, Z; Benmedakhene, S; Laksimi, A; Pluvinage, G.<br />

Modelling of damage and failure of glass/epoxy composite plates subject to impact<br />

fatigue. International Journal of Fatigue, 2001, 23, 877-885.<br />

[6] Schoeppner, GA; Abrate, S. Delamination threshold loads for low velocity impact on<br />

composite laminates. <strong>Composite</strong>s Part A, 2000, 31, 903-915.<br />

[8] Guden, M; Yildirim, U; Hall, IW. Effect of strain rate on the compression behaviour of a<br />

woven glass fiber/SC-15 composite. Polymer Testing, 2004, 23, 719-725.<br />

[9] Baucom, JN; Zikry, MA. Low-velocity impact damage progression in woven E-glass<br />

composite systems. <strong>Composite</strong>s Part A, 2005, 36, 658-664.<br />

[10] Ambu, R; Aymerich, F; Ginesu, F; Priolo, P. Assessment of NDT interferometric<br />

techniques for impact damage detection in composite laminates. <strong>Composite</strong>s Science and<br />

Technology, 2006, 66, 199-205.<br />

[11] Okoli, OI. The effect of strain rate and failure modes on the failure energy of fibre<br />

reinforced composites. <strong>Composite</strong> Structures, 2001, 54, 199-303.<br />

[12] Belingardi, G; Grasso, F; Vadori, R. Energy absorption and damage degree in impact<br />

testing of composite materials. Proceedings XI ICEM (Int. Conf. Experimental<br />

Mechanics), Oxford (UK), 1998, 279-285.<br />

[13] Belingardi, G; Vadori, R. Low velocity impact tests of laminate glass-fiber-epoxy matrix<br />

composite materials plates. International Journal of Impact Engineering, 2002, 27,<br />

213-229.

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