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Approximation of Linear Elastic Shells by Curved Triangular Finite Elements Based on Elastic Thick Shells Theory

机译:基于弹性厚壳理论的弯曲三角有限元近似线性弹性壳

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摘要

We have developed a curved finite element for a cylindrical thick shell based on the thick shell equations established in 1999 by Nzengwa and Tagne (N-T). The displacement field of the shell is interpolated from nodal displacements only and strains assumption. Numerical results on a cylindrical thin shell are compared with those of other well-known benchmarks with satisfaction. Convergence is rapidly obtained with very few elements. A scaling was processed on the cylindrical thin shell by increasing the ratio χ=h/2R (half the thickness over the smallest radius in absolute value) and comparing results with those obtained with the classical Kirchhoff-Love thin shell theory; it appears that results diverge at 2χ=1/10=0.316 because of the significant energy contribution of the change of the third fundamental form found in N-T model. This limit value of the thickness ratio which characterizes the limit between thin and thick cylindrical shells differs from the ratio 0.4 proposed by Leissa and 0.5 proposed by Narita and Leissa.
机译:我们开发了一种基于1999年的厚壳方程,由Nzengwa和Tagne(N-T)建立的厚壳方程开发了一种用于圆柱形厚壳的弯曲有限元。壳体的位移场仅从节点位移中插值并突出假设。将圆柱形薄壳上的数值结果与其他众所周知的基准的比较。用极少的元素迅速获得收敛。通过增加比率χ= H / 2R(绝对值最小半径的一半厚度)并将缩放在圆柱形薄壳上加工缩放,并将结果与​​用经典Kirchhoff-Love薄壳理论进行比较;由于N-T模型中发现的第三个基本形式的变化,因此似乎在2¼= 1/10 = 0.316处发散。这种厚度比的极限值,其表征薄圆柱形壳和厚圆柱形壳之间的极限不同于莱萨和莱萨提出的莱萨和0.5的比率0.4。

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