Thermally excited vibrations of aircraft structural elements


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Abstract

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.

About the authors

E. I. Starovoitov

Belarusian State University of Transport

Author for correspondence.
Email: edstar0@yandex.ru
Belarus, ul. Kirova 34, Gomel, 246653

D. V. Leonenko

Belarusian State University of Transport

Email: edstar0@yandex.ru
Belarus, ul. Kirova 34, Gomel, 246653

L. N. Rabinskii

Moscow Aviation Institute (National Research University)

Email: edstar0@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993

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