2002
DOI: 10.1016/s0022-5096(01)00101-6
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Buckling of nano-fibre reinforced composites: a re-examination of elastic buckling

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Cited by 78 publications
(52 citation statements)
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“…Furthermore, Su et al [17] studied the buckling behavior of multiple minerals in the nanostructure, considering the coupling of deformation among adjacent minerals. They showed that there are two typical buckling modes-one is antisymmetric mode which occurs at small aspect ratio, and the other one is symmetric mode which occurs at relatively large aspect ratio; for very large aspect ratio, the buckling strength of both symmetric and antisymmetric modes approached to that of continuous-fiber reinforced composite given by the Rosen model [18,19]. They also showed that the structural hierarchy enhances the buckling strength of biological materials.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, Su et al [17] studied the buckling behavior of multiple minerals in the nanostructure, considering the coupling of deformation among adjacent minerals. They showed that there are two typical buckling modes-one is antisymmetric mode which occurs at small aspect ratio, and the other one is symmetric mode which occurs at relatively large aspect ratio; for very large aspect ratio, the buckling strength of both symmetric and antisymmetric modes approached to that of continuous-fiber reinforced composite given by the Rosen model [18,19]. They also showed that the structural hierarchy enhances the buckling strength of biological materials.…”
Section: Introductionmentioning
confidence: 99%
“…This coupled, macro-to-micro approach revealed that one of the primary modeling obstacles was the selection of the relevant size of the representative volume element. Using a strictly continuum approach, Parnes, et al 5 modeled the influence of reinforcement volume fraction on inplane buckling of a composite plate. In Parnes study, it was assumed that carbon nanotube reinforced polymers would behave in a similar manner to the predicted behavior of dilute or low volume fraction composites.…”
Section: American Institute Of Aeronautics and Astronauticsmentioning
confidence: 99%
“…Ru [2000a;2000b] proposed the buckling analysis of CNTs with shell models. Parnes and Chiskis [2002] investigated elastic buckling of nanofiber reinforced composites with elastic beam theory. Wang and coworkers [Wang and Varadan 2005;Wang et al 2005b] have investigated global and local instability or kinks of CNTs with elastic beam models.…”
Section: Introductionmentioning
confidence: 99%