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The highest storage modulus was obtained for the 1% cellulose nanofibril reinforced pMDI-wood laminate sample.
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Experimental studies were conducted to characterize 24 layer plain weave graphite/epoxy laminate samples.
The unidirectional laminate samples were subjected to loading along 0° and 90° directions.
Experimental studies were conducted to characterize 24-layer satin weave graphite/epoxy laminate samples.
Six CFRP laminate samples with impact damages from 2 to 12 J were tested to verify the proposed methods.
The results predicted by the proposed fracture criterion are in a good agreement with the experimental observations on laminate samples.
Laminate samples are fabricated in the 90°/core/0° configuration for model validation.
The laminate samples were analyzed for viscoelastic properties using dynamic mechanical thermal analysis (DMTA).
Prior to numerical simulations, some experimental observations have been performed on the laminate samples in order to accurately represent the geometry of a periodic representative volume element (RVE).
Woven carbon/epoxy laminate samples were subjected to low-velocity impact loading at energy levels of 15, 30 and 45 J.
In this research, glass fibre reinforced composite laminate samples were manufactured with filament winding technique using four different vinyl ester resin systems to study ageing.
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