REFINED DISCRETE METHOD FOR CALCULATING STIFFENED ORTHOTROPIC SHELLS

Q3 Materials Science
A. Semenov
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引用次数: 0

Abstract

The author proposes a refined discrete method for taking into account stiffeners in the simulationof thin-walled shell structures. According to the method, it is necessary to add different reduction factors along different coordinate axes. For ribs directed perpendicular to the considered direction, a reduction factor is introduced equal to the ratio of the width of the ribs in this direction to the linear size of the shell in the considered direction. This method supplements the previously developed geometrically nonlinear mathematical model, which takes into account transverse shears and material orthotropy. The model is written as a functional of the total potential strain energy and can be used for different types of shells by specifying the Lame parameters and the radii of principal curvatures. The computational algorithm is based on the Ritz method and the method of continuation of the solution with respect to the best parameter. The software imple-mentation was carried out in the Maple software package. The applicability of the refined discrete method is shown by the example of orthotropic shallow shells of double curvature, simply supported along the contour and under the action of an external uniformly distributed transverse load. Material parameters were selected for T-10/UPE22-27 and 0/90 Woven Roving E-Glass/Vinyl Ester fiberglass. A comparison was made of the values of critical buckling loads for different stiffening options (a grid of ribs from 0 to 12 ribs in each direction) and a comparison of the values with the conventional discrete method, which showed that with the conventional discrete method, the values of buckling loads are significantly overestimated, especially with an increase in the number stiffening ribs. Comparison of the results of the test problem with the results of experiments obtained by other authors showed good agreement between the refined discrete method.
正交各向异性加劲壳的精细化离散计算方法
作者提出了一种在薄壁壳结构模拟中考虑加劲肋的精细离散方法。根据该方法,需要沿不同的坐标轴添加不同的折减因子。对于垂直于所考虑方向的肋条,引入的折减系数等于肋条在该方向上的宽度与壳体在所考虑方向上的线性尺寸之比。该方法补充了先前开发的几何非线性数学模型,该模型考虑了横向剪切和材料正交性。该模型被写成总势能的函数,通过指定Lame参数和主曲率半径,可以用于不同类型的壳体。计算算法基于Ritz方法和关于最佳参数的解的延拓方法。软件实现是在Maple软件包中进行的。通过正交各向异性双曲扁壳的例子表明了精细离散方法的适用性,该扁壳沿轮廓简单支撑,并在外部均匀分布的横向载荷作用下。选择T-10/UPE22-27和0/90机织粗纱E-玻璃纤维/乙烯基酯玻璃纤维的材料参数。对不同加劲方案(每个方向上从0到12个肋的肋网格)的临界屈曲载荷值进行了比较,并将这些值与传统离散方法进行了比较。结果表明,使用传统离散方法,屈曲载荷值被显著高估,尤其是随着加劲肋数量的增加。将测试问题的结果与其他作者获得的实验结果进行比较,表明改进的离散方法之间具有良好的一致性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
PNRPU Mechanics Bulletin
PNRPU Mechanics Bulletin Materials Science-Materials Science (miscellaneous)
CiteScore
1.10
自引率
0.00%
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0
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