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Postbuckling analysis of laminated composite plates subjected to in-plane uniaxial load

机译:面内单轴载荷下层合复合板的屈曲后分析

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摘要

The determination of critical buckling load of laminated composite plate is an important factor in determining the structural stability. This paper is concerned with the postbuckling behavior of a laminated composite plate uniaxially loaded in longitudinal direction for three different materials. The finite element software ABAQUS has been employed to analyze the laminated composite plates. Effects of different parameters such as fiber orientation angles, number of layers were examined. Results are presented in the form of plots showing the variation in non-dimensional buckling load with central deflection.
机译:层合复合板临界屈曲载荷的确定是决定结构稳定性的重要因素。本文关注的是在三种不同材料的纵向单轴加载的复合板的屈曲行为。有限元软件ABAQUS已用于分析层压复合板。检查了诸如纤维取向角,层数之类的不同参数的影响。结果以图的形式显示,显示了无量纲屈曲载荷随中心挠度的变化。

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