Thermally excited vibrations of aircraft structural elements
- Authors: Starovoitov E.I.1, Leonenko D.V.1, Rabinskii L.N.2
-
Affiliations:
- Belarusian State University of Transport
- Moscow Aviation Institute (National Research University)
- Issue: Vol 59, No 4 (2016)
- Pages: 466-473
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229844
- DOI: https://doi.org/10.3103/S106879981604005X
- ID: 229844
Cite item
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
Supplementary files
