Buckling and postbuckling behavior of shell type structures under thermo mechanical loads
| Autor: | V Ivana Vasovic, D Nenad Vidanovic, M Zoran Vasic, S Katarina Maksimovic, M Aleksandar Simonovic, S Mirko Maksimovic |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2021 |
| Předmět: |
post-buckling
Materials science Deformation (mechanics) Renewable Energy Sustainability and the Environment business.industry geometric non-linearity 020209 energy Composite number finite element method Shell (structure) 02 engineering and technology Structural engineering Composite laminates Finite element method Condensed Matter::Soft Condensed Matter Transverse plane shells Buckling thermal loads Thermal 0202 electrical engineering electronic engineering information engineering TJ1-1570 buckling Mechanical engineering and machinery business |
| Zdroj: | Thermal Science, Vol 25, Iss 6 Part A, Pp 4347-4357 (2021) |
| ISSN: | 2334-7163 0354-9836 |
| Popis: | The thermomechanical buckling and postbuckling behavior of layered composite shell type structure are considered with the finite element method (FEM) under the combination of temperature load and applied mechanical loads. To account for through-thickness shear deformation effects, the thermal elastic, Higher-Order Shear deformation Theory (HOST) is used in this study. The refined higher order theories, that takes into account the effect of transverse normal deformation, is used to develop discrete finite element models for the thermal buckling analysis of composite laminates. Attention in this study is focused on analyzing the temperature effects on buckling and postbuckling behavior of thin shell structural components. Special attention in this paper is focused on studying of values of the hole in curved panel on thermal buckling behavior and consequently to expend and upgrade previously conducted investigation. Using FEM, a broader observation of the critical temperature of loss of stability depending on the size of the hole was conducted. The presented numerical results based on HOST can be used as versatile and accurate method for buckling and postbuckling analyzes of thin-walled laminated plates under thermo-mechanical loads. |
| Databáze: | OpenAIRE |
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