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Glare, a fibre metal laminate (FML), consists of several thin 2014-T6 aerospace aluminium alloy layers alternately bonded with E-glass fibre based composite prepregs in the present work. As cracked Glare is subjected to load, load or fibre bridging over cracks in soft aluminium layers causes diversion of load away from the cracks towards stronger intact fibres in the prepregs resulting in stress reduction...
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