2013
DOI: 10.1007/s00466-013-0908-x
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Interface characteristics of carbon nanotube reinforced polymer composites using an advanced pull-out model

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Cited by 4 publications
(4 citation statements)
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“…(2009) [ 19 ]. Considering similar type of matrix, the result was further substantiated in terms of the force-displacement relationship trends that matches well with the result proposed by van Melick (2003) [ 8 ]. It can be seen from the Figure 10 that with the application of CNT, the force requirement for same indentation depth significantly increases compare to the pure epoxy polymer.…”
Section: Resultssupporting
confidence: 86%
See 2 more Smart Citations
“…(2009) [ 19 ]. Considering similar type of matrix, the result was further substantiated in terms of the force-displacement relationship trends that matches well with the result proposed by van Melick (2003) [ 8 ]. It can be seen from the Figure 10 that with the application of CNT, the force requirement for same indentation depth significantly increases compare to the pure epoxy polymer.…”
Section: Resultssupporting
confidence: 86%
“…Carbon nanotubes are considered as the key reinforcing element of high-performance nanocomposites [1,2,3,4,5,6]. Existing research suggests that the load carrying ability of composites can be improved significantly by the addition of carbon nanotubes or nano-ropes [4,7,8]. Chen et al (2004) observed in his study that an addition of 3.6% CNTs by volume in a matrix, the tensile stiffness of the nanocomposites can be increased by as much as 33% [4].…”
Section: Introductionmentioning
confidence: 99%
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“…Classical shear-lag model is widely used to obtain interface characteristics for fibre reinforced composite since 1950s. Recently, some researchers have extended the application of the shear-lag model for nanotube as well as nanorope (several CNT as bundle) reinforced composite using representative volume element (RVE) concept [14] [17]- [21]. Though there are some studies based on the interface fracture toughness to investigate interface cracking for fiber reinforced composite using shear-lag model, most of them consider the case of interface cracking of perfectly bonded interface to be debonded interface.…”
Section: Introductionmentioning
confidence: 99%