Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method

Buckling analysis of composite laminates under an in-plane compression load based on the mesh-free Galerkin Kriging method is presented. The moving Kriging interpolation (MK) technique possessing the delta property is employed to construct the shape functions, and thus no special techniques for impo...

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Main Author: Tinh Quoc Bui
Format: Article
Language:English
Published: Publishing House for Science and Technology 2011-06-01
Series:Vietnam Journal of Mechanics
Subjects:
Online Access:https://vjs.ac.vn/index.php/vjmech/article/view/39
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author Tinh Quoc Bui
author_facet Tinh Quoc Bui
author_sort Tinh Quoc Bui
collection DOAJ
description Buckling analysis of composite laminates under an in-plane compression load based on the mesh-free Galerkin Kriging method is presented. The moving Kriging interpolation (MK) technique possessing the delta property is employed to construct the shape functions, and thus no special techniques for imposing the essential boundary conditions are required. The present formulation is based on the Kirchhoff plate theory. The applicability, the accuracy and the effectiveness of the method are illustrated through a number of numerical examples. The results calculated by the proposed method are compared with those of existing reference solutions available in the literature and very good agreements are observed. It can be said that the proposed method can be considered as an alternative numerical technique in terms of meshfree methods.
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series Vietnam Journal of Mechanics
spelling doaj-art-a2f5df2a16fa4aabb8f534b15138aefd2025-08-20T03:04:43ZengPublishing House for Science and TechnologyVietnam Journal of Mechanics0866-71362815-58822011-06-0133210.15625/0866-7136/33/2/39Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free methodTinh Quoc Bui0University of SiegenBuckling analysis of composite laminates under an in-plane compression load based on the mesh-free Galerkin Kriging method is presented. The moving Kriging interpolation (MK) technique possessing the delta property is employed to construct the shape functions, and thus no special techniques for imposing the essential boundary conditions are required. The present formulation is based on the Kirchhoff plate theory. The applicability, the accuracy and the effectiveness of the method are illustrated through a number of numerical examples. The results calculated by the proposed method are compared with those of existing reference solutions available in the literature and very good agreements are observed. It can be said that the proposed method can be considered as an alternative numerical technique in terms of meshfree methods. https://vjs.ac.vn/index.php/vjmech/article/view/39bucklingcomposite laminatesmesh-free method
spellingShingle Tinh Quoc Bui
Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
Vietnam Journal of Mechanics
buckling
composite laminates
mesh-free method
title Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
title_full Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
title_fullStr Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
title_full_unstemmed Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
title_short Buckling analysis of simply supported composite laminates subjected to an in-plane compression load by a novel mesh-free method
title_sort buckling analysis of simply supported composite laminates subjected to an in plane compression load by a novel mesh free method
topic buckling
composite laminates
mesh-free method
url https://vjs.ac.vn/index.php/vjmech/article/view/39
work_keys_str_mv AT tinhquocbui bucklinganalysisofsimplysupportedcompositelaminatessubjectedtoaninplanecompressionloadbyanovelmeshfreemethod