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首页> 外文期刊>Russian Aeronautics >Stress-Strain State Analysis of Shells of Revolution Based on the Triangular Discretization Element with the Lagrange Multipliers
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Stress-Strain State Analysis of Shells of Revolution Based on the Triangular Discretization Element with the Lagrange Multipliers

机译:基于带有Lagrange乘数的三角离散元素的旋转壳体应力-应变状态分析

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摘要

The present paper sets forth an algorithm of analyzing thin shells with significant gradients of meridian curvature based on the Kirchhoff-Love hypothesis and finite element method. As a discretization element use is made of a triangular fragment of the middle surface with the Lagrange multipliers in additional nodes arranged in the triangle side middles. We apply the vector method of displacement interpolation that has a number of advantages over the conventional interpolation procedure. The high efficiency of the algorithm developed is confirmed by the numerical examples.
机译:本文提出了一种基于Kirchhoff-Love假设和有限元方法的,分析具有显着子午曲率梯度的薄壳的算法。作为离散化元素,可使用中间表面的三角形片段,而拉格朗日乘数位于布置在三角形中间的其他节点中。我们应用了位移插值的矢量方法,该方法比常规插值方法具有许多优势。数值例子证实了所开发算法的高效率。

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