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Buckling Analyses of Spherical Shells by the Finite Element Method Based on the Willis-Form Equations

机译:基于威利斯形式方程的有限元法屈曲分析球形壳

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Buckling analysis of spherical shells under external pressure is a crucial problem in mechanical and aerospace engineering. It is widely known that the buckling loads obtained by classical methods are much higher than experimental results. The main reason for this large discrepancy is customarily attributed to initial geometrical imperfections, and the impact of inhomogeneously distributed stresses during loading process is usually ignored. In order to investigate the effect of this ignored factor, the buckling loads of several spherical shells are analyzed by the geometrically nonlinear finite element method (FEM) based on the Willis-form equations, which explicitly contain the stress gradients at previous loading step. It can be shown that the buckling loads from the Willis-form FEM are about 10% lower than the values from classical FEM. This finding may give better understandings to the differences between theoretical and experimental results for nearly perfect spherical shells and may be helpful to obtain more accurate buckling loads for shells with initial geometrical imperfections.
机译:外部压力下球形壳的屈曲分析是机械和航空航天工程的关键问题。众所周知,通过经典方法获得的屈曲负荷远高于实验结果。这种大差异的主要原因是通常归因于初始几何缺陷的主要原因,通常忽略在装载过程中的不可均匀分布应力的影响。为了研究这种被忽略的因子的效果,基于基于威利斯形式的方程,通过几何非线性有限元方法(FEM)分析了几个球形壳的屈曲负荷,其在先前的加载步骤中明确地包含应力梯度。可以表明,来自威利斯形态有限元素的屈曲载荷比来自古典FEM的值低约10%。这一发现可能会更好地了解对几乎完美的球形壳的理论和实验结果之间的差异,并且可以有助于获得具有初始几何缺陷的壳体的更准确的屈曲负载。

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