Geometric nonlinear formulation of plate buckling structure

The analytical or exact mathematical formulation of stresses and displacements for plate buckling structure become impossible to develop if the plate geometry is so complicated. Numerical technique is one another approach to solve this problem and it is chosen in this study for plate structure under...

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Main Authors: Abu Bakar, S., Algaifi, H. A. A., Abd. Samat, R.
Format: Conference or Workshop Item
Language:English
Published: 2019
Subjects:
Online Access:http://eprints.utm.my/id/eprint/88764/1/SuhaimiAbuBakar2019_GeometricNonlinearFormulation.pdf
http://eprints.utm.my/id/eprint/88764/
https://dx.doi.org/10.1088/1755-1315/220/1/012022
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spelling my.utm.887642020-12-29T04:19:02Z http://eprints.utm.my/id/eprint/88764/ Geometric nonlinear formulation of plate buckling structure Abu Bakar, S. Algaifi, H. A. A. Abd. Samat, R. TA Engineering (General). Civil engineering (General) The analytical or exact mathematical formulation of stresses and displacements for plate buckling structure become impossible to develop if the plate geometry is so complicated. Numerical technique is one another approach to solve this problem and it is chosen in this study for plate structure under in-plane and out-plane load. The formulation of elastic stiffness matrix (ke) and geometric nonlinear stiffness matrix (kg) of the plate structure due to buckling is presented and based on virtual displacement principle. The geometric nonlinear stiffness matrix (kg) is found function of internal stresses. The direct iteration technique is applied to find nodal displacements. Under this technique, the Gauss points stresses are initialized as zeros, then the kg matrix is updated, and then a new nodal displacement vector is found for the next approximation of internal stresses. Iterative process is done until convergence of displacement is satisfied. The rectangular plate with one fixed edge supported is used to test the proposed nonlinear formulation and procedure. The compressive in-plane load and moment is considered and applied for the tested plate. The plate is discretized with appropriate number of triangular finite element mesh. It is found that, the convergence of displacement is satisfied by using direct iteration technique. The load - deflection curve shows nonlinear relationship and approach to critical load. This finding shows that the direct iteration method can be accepted for the analyzing of plate buckling by considering geometric nonlinear assumption. 2019 Conference or Workshop Item PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/88764/1/SuhaimiAbuBakar2019_GeometricNonlinearFormulation.pdf Abu Bakar, S. and Algaifi, H. A. A. and Abd. Samat, R. (2019) Geometric nonlinear formulation of plate buckling structure. In: 12th International Civil Engineering Post Graduate Conference, SEPKA 2018 and 3rd International Symposium on Expertise of Engineering Design, ISEED 2018, 27-28 Aug 2018, Johor, Malaysia. https://dx.doi.org/10.1088/1755-1315/220/1/012022
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TA Engineering (General). Civil engineering (General)
spellingShingle TA Engineering (General). Civil engineering (General)
Abu Bakar, S.
Algaifi, H. A. A.
Abd. Samat, R.
Geometric nonlinear formulation of plate buckling structure
description The analytical or exact mathematical formulation of stresses and displacements for plate buckling structure become impossible to develop if the plate geometry is so complicated. Numerical technique is one another approach to solve this problem and it is chosen in this study for plate structure under in-plane and out-plane load. The formulation of elastic stiffness matrix (ke) and geometric nonlinear stiffness matrix (kg) of the plate structure due to buckling is presented and based on virtual displacement principle. The geometric nonlinear stiffness matrix (kg) is found function of internal stresses. The direct iteration technique is applied to find nodal displacements. Under this technique, the Gauss points stresses are initialized as zeros, then the kg matrix is updated, and then a new nodal displacement vector is found for the next approximation of internal stresses. Iterative process is done until convergence of displacement is satisfied. The rectangular plate with one fixed edge supported is used to test the proposed nonlinear formulation and procedure. The compressive in-plane load and moment is considered and applied for the tested plate. The plate is discretized with appropriate number of triangular finite element mesh. It is found that, the convergence of displacement is satisfied by using direct iteration technique. The load - deflection curve shows nonlinear relationship and approach to critical load. This finding shows that the direct iteration method can be accepted for the analyzing of plate buckling by considering geometric nonlinear assumption.
format Conference or Workshop Item
author Abu Bakar, S.
Algaifi, H. A. A.
Abd. Samat, R.
author_facet Abu Bakar, S.
Algaifi, H. A. A.
Abd. Samat, R.
author_sort Abu Bakar, S.
title Geometric nonlinear formulation of plate buckling structure
title_short Geometric nonlinear formulation of plate buckling structure
title_full Geometric nonlinear formulation of plate buckling structure
title_fullStr Geometric nonlinear formulation of plate buckling structure
title_full_unstemmed Geometric nonlinear formulation of plate buckling structure
title_sort geometric nonlinear formulation of plate buckling structure
publishDate 2019
url http://eprints.utm.my/id/eprint/88764/1/SuhaimiAbuBakar2019_GeometricNonlinearFormulation.pdf
http://eprints.utm.my/id/eprint/88764/
https://dx.doi.org/10.1088/1755-1315/220/1/012022
_version_ 1687393618378096640
score 13.211869