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Examination of thermal postbuckling behavior of temperature dependent FG-GRMMC laminated plates with in-plane negative Poisson’s ratio
Abstract Auxetic composite laminates are a new type of engineering materials that have unique features for important potential applications. This paper examines the effect of in-plane negative Poisson’s ratio (NPR) on the thermal postbuckling behaviors of graphene-reinforced metal matrix composite (GRMMC) plates. The plates rest on an elastic foundation and are subjected to a uniform temperature rise. The GRMMC layers with different volume fractions of graphene reinforcement can be arranged to achieve piece-wise functionally graded (FG) patterns across the plate thickness and the material properties of the GRMMC layers are temperature-dependent. The Reddy’s third order shear deformation plate theory and the geometric nonlinearity of von Kármán-type are applied to formulate the thermal postbuckling equations for GRMMC laminated plates. The nonlinear problem can be solved by a two-step perturbation approach. Parametric study is performed for () and () GRMMC laminated plates possessing in-plane NPR. The results reveal that the buckling temperatures for () and () plates are significantly enhanced with an FG-X pattern for the plates. We found that due to the combined effect of FG and in-plane NPR, the thermal postbuckling strength of FG-X () plate is higher than that of FG-X () plate.
Highlights Thermal buckling of auxetic GRMMC laminated plates is presented for the first time. Both in-plane negative Poisson’s ratios and functionally graded patterns are considered. The material properties of GRMMC layer are anisotropic and temperature dependent. The new findings for the thermal postbuckling behaviors of GRMMC laminated plates are presented.
Examination of thermal postbuckling behavior of temperature dependent FG-GRMMC laminated plates with in-plane negative Poisson’s ratio
Abstract Auxetic composite laminates are a new type of engineering materials that have unique features for important potential applications. This paper examines the effect of in-plane negative Poisson’s ratio (NPR) on the thermal postbuckling behaviors of graphene-reinforced metal matrix composite (GRMMC) plates. The plates rest on an elastic foundation and are subjected to a uniform temperature rise. The GRMMC layers with different volume fractions of graphene reinforcement can be arranged to achieve piece-wise functionally graded (FG) patterns across the plate thickness and the material properties of the GRMMC layers are temperature-dependent. The Reddy’s third order shear deformation plate theory and the geometric nonlinearity of von Kármán-type are applied to formulate the thermal postbuckling equations for GRMMC laminated plates. The nonlinear problem can be solved by a two-step perturbation approach. Parametric study is performed for () and () GRMMC laminated plates possessing in-plane NPR. The results reveal that the buckling temperatures for () and () plates are significantly enhanced with an FG-X pattern for the plates. We found that due to the combined effect of FG and in-plane NPR, the thermal postbuckling strength of FG-X () plate is higher than that of FG-X () plate.
Highlights Thermal buckling of auxetic GRMMC laminated plates is presented for the first time. Both in-plane negative Poisson’s ratios and functionally graded patterns are considered. The material properties of GRMMC layer are anisotropic and temperature dependent. The new findings for the thermal postbuckling behaviors of GRMMC laminated plates are presented.
Examination of thermal postbuckling behavior of temperature dependent FG-GRMMC laminated plates with in-plane negative Poisson’s ratio
Shen, Hui-Shen (author) / Xiang, Y. (author)
Thin-Walled Structures ; 163
2021-04-04
Article (Journal)
Electronic Resource
English
Thermal Postbuckling of Laminated Composite Plates with Temperature Dependent Properties
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