单壁碳纳米管轴向屈曲的非局部fluge壳模型:一种解析方法

IF 1.2 Q4 NANOSCIENCE & NANOTECHNOLOGY
R. Ansari, H. Rouhi
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引用次数: 19

摘要

研究了单壁碳纳米管(SWCNTs)在轴向载荷作用下的稳定性。为此,建立了一个非局部Flugge壳模型,以适应小长度尺度效应。采用带梁函数的解析瑞利-里兹方法求解fluge型屈曲方程的变分表达式。通过分子动力学(MD)模拟,获得了(8,8)扶手型SWCNTs在不同末端条件下的临界轴向屈曲载荷。通过本文解析解与分子动力学模拟结果的比较,提出了不同边界条件下SWCNTs非局部参数的合适取值。研究了非局部参数和边界条件对临界屈曲载荷的影响。此外,尽管在定义纳米管的面内刚度和弯曲刚度时存在不确定性,但通过调整非局部参数,所建立的非局部壳模型能够预测MD模拟结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
NONLOCAL FLUGGE SHELL MODEL FOR THE AXIAL BUCKLING OF SINGLE-WALLED CARBON NANOTUBES: AN ANALYTICAL APPROACH
In this paper, the stability characteristics of single-walled carbon nanotubes (SWCNTs) under the action of axial load are investigated. To this end, a nonlocal Flugge shell model is developed to accommodate the small length scale effects. The analytical Rayleigh-Ritz method with beam functions is applied to the variational statement derived from the Flugge-type buckling equations. Molecular dynamics (MD) simulations are performed to obtain the critical axial buckling loads of (8,8) armchair SWCNTs with different types of end conditions. Through comparison of the results obtained from the present analytical solution and the ones from molecular dynamics simulations, the appropriate values of nonlocal parameter are proposed for SWCNTs with different kinds of boundary conditions. The effects of nonlocal parameter and boundary conditions on the critical buckling load are also examined. Moreover, in spite of the uncertainty that exists in defining the in-plane stiffness and bending rigidity of nanotube, by adjusting the nonlocal parameter, the present nonlocal shell model is shown to be capable of predicting the MD simulations results.
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来源期刊
international journal of nano dimension
international journal of nano dimension NANOSCIENCE & NANOTECHNOLOGY-
CiteScore
2.80
自引率
20.00%
发文量
0
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