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首页> 外文期刊>Russian Aeronautics >Stress-Strain Analysis of a Thin-Shell Part of Fuselage Using a Triangular Finite Element with Lagrange Multipliers
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Stress-Strain Analysis of a Thin-Shell Part of Fuselage Using a Triangular Finite Element with Lagrange Multipliers

机译:用拉格朗日乘数三角有限元的机身薄壳部分的应力 - 应变分析

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摘要

We developed a triangular discretization element of the fuselage fragment in the form of a thin shell compatible with the adjacent elements based on Lagrange multipliers. Solution of several test problems showed a high efficiency of using the modification of a triangular finite element being proposed.
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