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Computational Analysis Based on Creep Damage Mechanics for Creep Bifurcation Buckling of Circular Cylindrical Shell Subjected to Axial Compression

机译:基于蠕变损伤力学的圆柱壳轴压蠕变分叉屈曲计算分析

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摘要

Cylindrical shells are utilized as structural elements of nuclear power plants, heat exchangers or pressure vessels, which are operated under elevated temperature. Creep buckling is one of the failure modes of structures at elevated temperature. In some experiments conducted by other authors, axially compressive cylindrical shells with a large ratio of radius to thickness were observed to buckle with circumferential waves. We reported that the circumferential waves occur due to bifurcation buckling. But, the critical time and the minimum loading for bifurcation buckling obtained from calculations of finite element analyses are not very good agreement with those of the experiments. One of the reasons for the disagreement is considered to be that the creep constitutive equations employed in many previous analyses represent steady creep. The creep phenomena usually have primary creep period, steady creep one and tertiary creep one. A creep strain-time relation through the three periods can be simulated by using a constitutive equation based on creep damage meachanics. In the present paper, we analyze bifurcation creep buckling of circular cylindrical shells subjected to axial compression by the use of the finite element method taking account of the creep damage mechanics of Kachanov-Rabotnov.
机译:圆柱壳被用作在高温下运行的核电站,热交换器或压力容器的结构元件。蠕变屈曲是结构在高温下的破坏模式之一。在其他作者进行的一些实验中,观察到半径与厚度之比大的轴向压缩圆柱壳在周波作用下弯曲。我们报道周波是由于分叉屈曲而产生的。但是,通过有限元分析计算得出的临界时间和分叉屈曲的最小载荷与实验结果并不十分吻合。出现分歧的原因之一是,许多先前分析中采用的蠕变本构方程表示稳态蠕变。蠕变现象通常具有一次蠕变周期,一次稳定蠕变和三次蠕变。可以通过使用基于蠕变损伤机理的本构方程来模拟三个周期的蠕变应变时间关系。在本文中,我们考虑到Kachanov-Rabotnov的蠕变损伤机理,使用有限元方法分析了承受轴向压缩的圆柱壳的分叉蠕变屈曲。

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