2016
DOI: 10.1016/j.compositesa.2016.02.003
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Assessment of carbon nanotube yarns as reinforcement for composite overwrapped pressure vessels

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Cited by 48 publications
(34 citation statements)
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“…The CNT bundles are not curved so ϕ is zero, and the maximum holding stress must equal the frictional shear stress (T f ric ) between the nanotubes. For the purpose of this discussion, the tensile stress inside the CNT network is estimated using Equation (1). In this case, the twisted yarns exhibit a UTS of 0.8 GPa, so considering this as T Load means T Hold could only apply 0.8 GPa to the nanotube to prevent the pullout.…”
Section: Strengthening Mechanismmentioning
confidence: 99%
See 1 more Smart Citation
“…The CNT bundles are not curved so ϕ is zero, and the maximum holding stress must equal the frictional shear stress (T f ric ) between the nanotubes. For the purpose of this discussion, the tensile stress inside the CNT network is estimated using Equation (1). In this case, the twisted yarns exhibit a UTS of 0.8 GPa, so considering this as T Load means T Hold could only apply 0.8 GPa to the nanotube to prevent the pullout.…”
Section: Strengthening Mechanismmentioning
confidence: 99%
“…Carbon nanotubes (CNTs) have unique structures and properties that could be advantageous in forming composites for structural applications [1,2], flexible sensing substrates [3], and multi-functional devices [4]. The ultimate tensile strength (UTS) of a carbon nanotube has been measured to be 150 GPa [5].…”
Section: Introductionmentioning
confidence: 99%
“…Carbon nanotubes (CNTs), for example, have been shown by modeling and nano/micro-scale measurements to have much higher specific strength and stiffness than carbon fibers [2][3][4]. In recent years, rapid advances in manufacturing and processing have led to the availability of large quantities of high quality CNTs in practically useful material formats, such as large sheets and kilometerlength yams [5][6][7]. As a result, it is now possible to fabricate high volume fraction CNT composites with specific strength and stiffness values that approach those of current aerospace carbon fiber composites [6][7][8][9].…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, rapid advances in manufacturing and processing have led to the availability of large quantities of high quality CNTs in practically useful material formats, such as large sheets and kilometerlength yams [5][6][7]. As a result, it is now possible to fabricate high volume fraction CNT composites with specific strength and stiffness values that approach those of current aerospace carbon fiber composites [6][7][8][9]. These properties are achieved in samples with notably non-optimal microstructures: they exhibit large voids, both within and between the reinforcing yarns [6].…”
Section: Introductionmentioning
confidence: 99%
“…While many more applications have been cited for this versatile material, its insertion into real missions is still limited (De Volder et al, 2013). Only recent advancements in large-scale manufacturing of this material has permitted a broader assessment of their utility in aerospace applications (Gurau, 2014;Alvarez et al, 2015;Kim et al, 2016;DexMat Carbon, 2017;Space Technology, 2016). Focused development of this material can be aided by the prioritization of its utility in various mission scenarios that require the development of advanced materials to come to fruition.…”
Section: Introductionmentioning
confidence: 99%