Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations

Nonlinear stability of nanocomposite spherical and cylindrical panels reinforced by carbon nanotubes (CNTs), resting on elastic foundations and subjected to uniform external pressure in thermal environments is investigated in this paper. CNTs are embedded into matrix phase through uniform distributi...

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Main Authors: Trang Le Thi Nhu, Tung Hoang Van
Format: Article
Language:English
Published: De Gruyter 2019-01-01
Series:Nonlinear Engineering
Subjects:
Online Access:https://doi.org/10.1515/nleng-2018-0077
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spelling doaj-7ce8c5e69e5d4323aae4a995b501dc9a2021-09-06T19:21:07ZengDe GruyterNonlinear Engineering2192-80102192-80292019-01-018158259610.1515/nleng-2018-0077nleng-2018-0077Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundationsTrang Le Thi Nhu0Tung Hoang Van1Faculty of Civil Engineering, University of Transport Technology, Ha Noi, Viet NamFaculty of Civil Engineering, Hanoi Architectural University, Ha Noi, Viet NamNonlinear stability of nanocomposite spherical and cylindrical panels reinforced by carbon nanotubes (CNTs), resting on elastic foundations and subjected to uniform external pressure in thermal environments is investigated in this paper. CNTs are embedded into matrix phase through uniform distribution (UD) or functionally graded (FG) distribution, and effective properties of CNT-reinforced composite are estimated through an extended rule of mixture. Governing equations are based on classical shell theory taking geometrical nonlinearity, initial geometrical imperfection and panel-foundation interaction into consideration. Approximate solutions of deflection and stress functions are assumed to satisfy simply supported boundary conditions and Galerkin method is applied to obtain nonlinear load-deflection relation. Numerical examples show the effects of volume fraction and distribution type of CNTs, in-plane condition of edges, curvature of panel, thermal environments, elastic foundations and imperfection size on the nonlinear response and snap-through instability of the curved panels. The present study reveals that efficiency of CNT distribution type depends on curvature of panel and in-plane behavior of boundary edges, and bifurcation type buckling response of pressure-loaded panels may occur at elevated temperature.https://doi.org/10.1515/nleng-2018-0077doubly curved panelcnt-reinforced compositethermomechanical loadingnonlinear stabilityelastic foundation
collection DOAJ
language English
format Article
sources DOAJ
author Trang Le Thi Nhu
Tung Hoang Van
spellingShingle Trang Le Thi Nhu
Tung Hoang Van
Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
Nonlinear Engineering
doubly curved panel
cnt-reinforced composite
thermomechanical loading
nonlinear stability
elastic foundation
author_facet Trang Le Thi Nhu
Tung Hoang Van
author_sort Trang Le Thi Nhu
title Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
title_short Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
title_full Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
title_fullStr Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
title_full_unstemmed Thermomechanical nonlinear stability of pressure-loaded CNT-reinforced composite doubly curved panels resting on elastic foundations
title_sort thermomechanical nonlinear stability of pressure-loaded cnt-reinforced composite doubly curved panels resting on elastic foundations
publisher De Gruyter
series Nonlinear Engineering
issn 2192-8010
2192-8029
publishDate 2019-01-01
description Nonlinear stability of nanocomposite spherical and cylindrical panels reinforced by carbon nanotubes (CNTs), resting on elastic foundations and subjected to uniform external pressure in thermal environments is investigated in this paper. CNTs are embedded into matrix phase through uniform distribution (UD) or functionally graded (FG) distribution, and effective properties of CNT-reinforced composite are estimated through an extended rule of mixture. Governing equations are based on classical shell theory taking geometrical nonlinearity, initial geometrical imperfection and panel-foundation interaction into consideration. Approximate solutions of deflection and stress functions are assumed to satisfy simply supported boundary conditions and Galerkin method is applied to obtain nonlinear load-deflection relation. Numerical examples show the effects of volume fraction and distribution type of CNTs, in-plane condition of edges, curvature of panel, thermal environments, elastic foundations and imperfection size on the nonlinear response and snap-through instability of the curved panels. The present study reveals that efficiency of CNT distribution type depends on curvature of panel and in-plane behavior of boundary edges, and bifurcation type buckling response of pressure-loaded panels may occur at elevated temperature.
topic doubly curved panel
cnt-reinforced composite
thermomechanical loading
nonlinear stability
elastic foundation
url https://doi.org/10.1515/nleng-2018-0077
work_keys_str_mv AT tranglethinhu thermomechanicalnonlinearstabilityofpressureloadedcntreinforcedcompositedoublycurvedpanelsrestingonelasticfoundations
AT tunghoangvan thermomechanicalnonlinearstabilityofpressureloadedcntreinforcedcompositedoublycurvedpanelsrestingonelasticfoundations
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