DocumentCode :
2333813
Title :
Predicting a stretching behavior of carbon nanotubes using finite element method
Author :
Mohammadpour, E. ; Awang, M.
Author_Institution :
Mech. Eng. Dept., Univ. Teknol. PETRONAS, Seri Iskandar, Malaysia
fYear :
2010
fDate :
1-3 Dec. 2010
Firstpage :
1
Lastpage :
2
Abstract :
This paper describes a finite element method that is appropriate for the numerical prediction of the nonlinear mechanical behavior of different types of isolated single walled carbon nanotubes. A finite element progressive fracture model based on the modified Morse interatomic potential is used to evaluate mechanical properties of carbon nanotubes, such as axial and radial Young´s modulus, shear modulus, natural frequency and buckling load are presented to illustrate the accuracy of this simulation technique. The novelty of the model lies on the use of beam element with non-linear capability, i.e, BEAM188, to evaluate SWNTs mechanical properties. In the present modeling work, individual carbon nanotube is simulated as a frame-like structure and the primary bonds between two nearest-neighboring atoms are treated as 3D beam elements. The beam element nonlinear properties are determined via the concept of energy equivalence between molecular dynamics and structural mechanics using Modified Morse potential.
Keywords :
Morse potential; Young´s modulus; buckling; carbon nanotubes; finite element analysis; fracture; molecular dynamics method; shear modulus; 3D beam elements; C; Morse interatomic potential; Young´s modulus; buckling load; finite element method; finite element progressive fracture model; isolated single walled carbon nanotubes; molecular dynamics; nonlinear mechanical properties; shear modulus; stretching property; structural mechanics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Enabling Science and Nanotechnology (ESciNano), 2010 International Conference on
Conference_Location :
Kuala Lumpur
Print_ISBN :
978-1-4244-8853-7
Type :
conf
DOI :
10.1109/ESCINANO.2010.5701056
Filename :
5701056
Link To Document :
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