2009
DOI: 10.1002/adfm.200900011
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Increased Interface Strength in Carbon Fiber Composites through a ZnO Nanowire Interphase

Abstract: One of the most important factors in the design of a fiber reinforced composite is the quality of the fiber/matrix interface. Recently carbon nanotubes and silicon carbide whiskers have been used to enhance the interfacial properties of composites; however, the high growth temperature degrade the fiber strength and significantly reduce the composite's in‐plane properties. Here, a novel method for enhancing the fiber/matrix interfacial strength that does not degrade the mechanical properties of the fiber is dem… Show more

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Cited by 218 publications
(189 citation statements)
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“…The major benefits are: no or less reduction of the substrate fiber tensile properties, growth at relatively low temperature, and possibility of achieving multifunctionality. In fact, ZnO display piezoelectric and semiconductor properties, which may be exploited in advanced composites for sensing applications [80].…”
Section: Grafting By Non-carbon Nanofibersmentioning
confidence: 99%
“…The major benefits are: no or less reduction of the substrate fiber tensile properties, growth at relatively low temperature, and possibility of achieving multifunctionality. In fact, ZnO display piezoelectric and semiconductor properties, which may be exploited in advanced composites for sensing applications [80].…”
Section: Grafting By Non-carbon Nanofibersmentioning
confidence: 99%
“…The number of fragments is directly related to the interfacial shear strength and is shown to significantly increase in Figure 1. The interfacial shear strength can be computed from the average fragment length and was observed to increase from 15.87 MPa to 33.87 MPa 32 or by 113%. The increase is attributed to increased surface area, mechanical interlocking and a gradient of mechanical properties between the dissimilar materials.…”
Section: Resultsmentioning
confidence: 99%
“…ZnO nanowire arrays were grown on functionalized aramid fibers through the same procedure used with carbon fibers. 32,[35][36][37][38] To prepare single fiber fragmentation samples, single aramid fibers were placed in a silicone rubber mold (3120 RTV; Dow Corning, Midland, MI) and preloaded to 15 g, for the same reason discussed before. The molds were then filled with a 100:16.9 mixture of Epon 862/Epikure 9553 (Hexion, Houston, TX) and gelled for 1 h. The molds were heated in an oven to 100°C for 1 h, followed by 1 h at 160°C.…”
Section: Methodsmentioning
confidence: 99%
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