Email this article Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
- Authors: Zheleznov L.P.1, Kabanov V.V.1, Boiko D.V.1
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Affiliations:
- Chaplygin Aeronautical Research Institute (SibNIA)
- Issue: Vol 61, No 2 (2018)
- Pages: 175-182
- Section: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230472
- DOI: https://doi.org/10.3103/S1068799818020046
- ID: 230472
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Abstract
The problem of strength and stability of shells under torsion and internal pressure was solved. It was found out the influence of the internal pressure, ellipticity and nonlinearity of deformation on the critical buckling load of the shell.
About the authors
L. P. Zheleznov
Chaplygin Aeronautical Research Institute (SibNIA)
Author for correspondence.
Email: lev.sheleznov@ocrv.ru
Russian Federation, ul. Polzunova 21, Novosibirsk, 630051
V. V. Kabanov
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Russian Federation, ul. Polzunova 21, Novosibirsk, 630051
D. V. Boiko
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Russian Federation, ul. Polzunova 21, Novosibirsk, 630051
