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The analysis of failure surface indicated that the failure modes of Cf/Mg composites were mainly shear failure and delamination failure.
The physicomechanical properties of the polyolefin/RGO composites were mainly determined by the interplay of two influence factors: exfoliation degree (specific surface area) and modification degree.
As shown in Fig. 1c, f, i and Table S1, all three composites were mainly comprised of cobalt and oxygen, with trace amounts of carbon and nitrogen.
On the basis of these results, it could be concluded that the pores in the Co3O4/NPC composites were mainly mesopores.
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The properties of fiber reinforced composites are mainly determined by the fraction of reinforcement and matrix.
Damage induced by laser shock testing in carbon-basalt woven fabric/epoxy composites is mainly inter-ply delamination.
The superior lithium storage performance of the pseudo-solid-solution CuCo2O4/C composites is mainly attributed to the unique amorphous structure.
The matrix phase of composites is mainly composed of ordinary Portland cement (OPC), Metakaolin (M), and limestone powder, respectively.
Carbon FRP CFRPP) composites are mainly used for EBR applications whereas glass FRP GFRPP) bars are employed as internal reinforcement of concrete elements.
Results show that the effect of matrix type on the friction and wear properties of the composites is mainly related to its hardness and binding property with graphite.
Nanocomposites are widely applied in many fields of science however, cement-based composites are mainly modified with single type of nanostructures.
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