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Elastic limit load prediction and equivalent cylinder proposal for circular concave shells subjected to axial compression

机译:弹性限制负载预测和对轴向压缩的圆形凹壳的等效气缸提案

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The paper aims to propose an equivalent cylinder radius approach for circular cross-section concave shells under axial compression. Several buckling relations are introduced to predict critical stresses and to limit loads considering the extensive range of geometrical parameters. A detailed parametric study is conducted to reveal the influence of concavity on critical stress using geometrically nonlinear analysis (GNA). The amount of reduction in limit load of a concave shell, as a reference to an ideal case, is expressed as a function meridional curvature. An asymmetry factor is described to evaluate the change of critical stresses for longitudinally asymmetric concave shells. A similarity approach is given for the concave shells. A statistical procedure is utilized to examine the accuracy of the equations and relatively satisfactory results are achieved.
机译:纸张旨在提出轴向压缩下圆形横截面的等效气缸半径方法。 引入了几个屈曲关系以预测临界应力并限制考虑到广泛的几何参数范围的负荷。 进行详细的参数研究以揭示使用几何非线性分析(GNA)的凹陷对临界应力的影响。 凹形壳的限制负荷的减少量,作为理想情况的参考,表示为函数子午线曲率。 描述了不对称因子来评估纵向不对称凹壳的临界应力的变化。 给出了凹形壳的相似性方法。 利用统计程序来检查方程的准确性和相对令人满意的结果。

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