Molecular Dynamics Simulations and Theoretical Model for Engineering Tensile Properties of Single-and Multi-Walled Carbon Nanotubes.

carbon nanotube defect density mechanical properties molecular dynamics simulations tensile strength

Journal

Nanomaterials (Basel, Switzerland)
ISSN: 2079-4991
Titre abrégé: Nanomaterials (Basel)
Pays: Switzerland
ID NLM: 101610216

Informations de publication

Date de publication:
19 Mar 2021
Historique:
received: 19 02 2021
revised: 11 03 2021
accepted: 17 03 2021
entrez: 3 4 2021
pubmed: 4 4 2021
medline: 4 4 2021
Statut: epublish

Résumé

To apply carbon nanotubes (CNTs) as reinforcing agents in next-generation composites, it is essential to improve their nominal strength. However, since it is difficult to completely remove the defects, the synthesis guideline for improving nominal strength is still unclear, i.e., the effective strength and the number of nanotube layers required to improve the nominal strength has been undermined. In this study, molecular dynamics simulations were used to elucidate the effects of vacancies on the mechanical properties of CNTs. Additionally, the relationships between the number of layers and effective and nominal strengths of CNTs were discussed theoretically. The presence of extensive vacancies provides a possible explanation for the low nominal strengths obtained in previous experimental measurements of CNTs. This study indicates that the nominal strength can be increased from the experimentally obtained values of 10 GPa to approximately 20 GPa by using six to nine nanotube layers, even if the increase in effective strength of each layer is small. This has advantages over double-walled CNTs, because the effective strength of such CNTs must be approximately 60 GPa to achieve a nominal strength of 20 GPa.

Identifiants

pubmed: 33808899
pii: nano11030795
doi: 10.3390/nano11030795
pmc: PMC8003771
pii:
doi:

Types de publication

Journal Article

Langues

eng

Subventions

Organisme : Japan Society for the Promotion of Science
ID : JP19K14837

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Auteurs

Keiichi Shirasu (K)

Department of Aerospace Engineering, Tohoku University, 6-6-01, Aza-Aoba, Aramaki, Aobaku, Sendai, Miyagi 980-8579, Japan.

Shunsuke Kitayama (S)

Fracture and Reliability Research Institute, Tohoku University, 6-6-11, Aza-Aoba, Aramaki, Aobaku, Sendai, Miyagi 980-8579, Japan.

Fan Liu (F)

Fracture and Reliability Research Institute, Tohoku University, 6-6-11, Aza-Aoba, Aramaki, Aobaku, Sendai, Miyagi 980-8579, Japan.

Go Yamamoto (G)

Department of Aerospace Engineering, Tohoku University, 6-6-01, Aza-Aoba, Aramaki, Aobaku, Sendai, Miyagi 980-8579, Japan.
School of Mechanical Engineering, Sungkyunkwan University, Suwon 16419, Korea.

Toshiyuki Hashida (T)

Fracture and Reliability Research Institute, Tohoku University, 6-6-11, Aza-Aoba, Aramaki, Aobaku, Sendai, Miyagi 980-8579, Japan.

Classifications MeSH