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Thermally excited vibrations of aircraft structural elements

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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Published in:Russian aeronautics 2016-10, Vol.59 (4), p.466-473
Main Authors: Starovoitov, E. I., Leonenko, D. V., Rabinskii, L. N.
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Language:English
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container_end_page 473
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container_start_page 466
container_title Russian aeronautics
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creator Starovoitov, E. I.
Leonenko, D. V.
Rabinskii, L. N.
description 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.
doi_str_mv 10.3103/S106879981604005X
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ispartof Russian aeronautics, 2016-10, Vol.59 (4), p.466-473
issn 1068-7998
1934-7901
language eng
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source Springer Nature
subjects Aircraft
Aircraft components
Aircraft vibration
Automotive Engineering
Engineering
Numerical analysis
Structural Mechanics and Strength of Flight Vehicles
Structural members
Thermal shock
title Thermally excited vibrations of aircraft structural elements
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