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The efficiency of the composites is mainly affected by the amount of Ce3+ species on the surface.
Damage induced by laser shock testing in carbon-basalt woven fabric/epoxy composites is mainly inter-ply delamination.
The matrix phase of composites is mainly composed of ordinary Portland cement (OPC), Metakaolin (M), and limestone powder, respectively.
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.
This move towards composites is mainly because of the increased mechanical performance, less corrosion and fatigue problems, allowing for longer service life of the aircraft.
The superior lithium storage performance of the pseudo-solid-solution CuCo2O4/C composites is mainly attributed to the unique amorphous structure.
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Textural analysis shows that initial silica is mainly meso/macroporous, but composites are mainly macroporous.
The properties of fiber reinforced composites are mainly determined by the fraction of reinforcement and matrix.
On the basis of these results, it could be concluded that the pores in the Co3O4/NPC composites were mainly mesopores.
This is very important because most of the fascinating properties of graphene-based composites are mainly related with their layer numbers of graphene.
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.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com