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Buckling of circular/annular Mindlin nanoplates via nonlocal elasticity

机译:通过非局部弹性使圆形/环形Mindlin纳米板屈曲

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摘要

The present study proposes an analytical solution for the axisymmetric/asymmetric buckling analysis of moderately thick circular/annular Mindlin nanoplates under uniform radial compressive in-plane load. In order to consider small-scale effects, nonlocal elasticity theory of Eringen is employed. To ensure the efficiency and stability of the present methodology, the results are compared with other ones presented in the literature. Further the exact closed-form solution is obtained using three potential functions. In addition, the effect of small scales on buckling loads for different parameters such as geometry of the nanoplate, boundary conditions, and axisymmetric/asymmetric mode numbers, is investigated. It is observed that the buckling mode shape for annular nanoplates, which corresponds to the lowest critical buckling load, may be axisymmetric or asymmetric depending on boundary conditions, inner to outer radius ratios, and thickness of the nanoplate. In other words, for stiffer boundary conditions and smaller inner to outer radius ratios, the mode shape corresponding to the lowest critical buckling load is an asymmetric mode. Also, the difference between axisymmetric and asymmetric buckling loads for higher mode numbers, greater thickness to outer radius ratios and smaller outer radii decreases by increasing the nonlocal parameter.
机译:本研究为中等厚度的圆形/环形Mindlin纳米板在均匀径向压缩面内载荷下的轴对称/不对称屈曲分析提出了一种解析解。为了考虑小范围的影响,采用了艾林根的非局部弹性理论。为了确保本方法的效率和稳定性,将结果与文献中提供的其他结果进行比较。此外,使用三个势函数可以获得精确的封闭形式解。另外,研究了小尺度对不同参数(例如纳米板的几何形状,边界条件和轴对称/不对称模数)的屈曲载荷的影响。观察到,对应于最低临界屈曲载荷的环形纳米板的屈曲模式形状可以是轴对称的或不对称的,这取决于边界条件,内外半径比和纳米板的厚度。换句话说,对于较硬的边界条件和较小的内外半径比,与最低临界屈曲载荷相对应的模态为非对称模态。同样,通过增加非局部参数,轴对称和非对称屈曲载荷之间的差异对于更高的模数,更大的厚度与外半径比以及更小的外半径会减小。

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