Investigation of Buckling Behavior for Thin-Walled Bearing Aircraft Structural Elements with Cutouts by Means of Numerical Simulation


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In this paper, we develop the consistent mathematical models and appropriate lowconsuming numerical methods for investigating the nonlinear strain and buckling behavior of statically loaded thin-walled structures with cutouts. The numerical simulation allowed us to study the effects of the dimensions of rectangular cutouts on the buckling of cylindrical shells loaded by the external pressure.

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V. Dmitriev

Moscow Aviation Institute (National Research University)

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Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

O. Egorova

Moscow Aviation Institute (National Research University)

Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

S. Zhavoronok

Institute of Applied Mechanics

Email: vgd2105@mail.ru
俄罗斯联邦, Leningradskii pr. 7, Moscow, 125040

L. Rabinskii

Moscow Aviation Institute (National Research University)

Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993

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