Thermally excited vibrations of aircraft structural elements


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This paper considers the axisymmetric transverse vibrations of aircraft nonuniform structural elements that are introduced by a thermal shock. Analytical solutions have been obtained and their numerical analysis has been performed.

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E. Starovoitov

Belarusian State University of Transport

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Email: edstar0@yandex.ru
白俄罗斯, ul. Kirova 34, Gomel, 246653

D. Leonenko

Belarusian State University of Transport

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白俄罗斯, ul. Kirova 34, Gomel, 246653

L. Rabinskii

Moscow Aviation Institute (National Research University)

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俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993

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