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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 |
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Language: | English |
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container_end_page | 473 |
container_issue | 4 |
container_start_page | 466 |
container_title | Russian aeronautics |
container_volume | 59 |
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 |
format | article |
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identifier | ISSN: 1068-7998 |
ispartof | Russian aeronautics, 2016-10, Vol.59 (4), p.466-473 |
issn | 1068-7998 1934-7901 |
language | eng |
recordid | cdi_proquest_journals_2063661800 |
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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