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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Bibliographic Details
Published in:Russian aeronautics 2016-10, Vol.59 (4), p.466-473
Main Authors: Starovoitov, E. I., Leonenko, D. V., Rabinskii, L. N.
Format: Article
Language:English
Subjects:
Aircraft
Aircraft components
Aircraft vibration
Automotive Engineering
Engineering
Numerical analysis
Structural Mechanics and Strength of Flight Vehicles
Structural members
Thermal shock
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Description
Summary: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S106879981604005X