Free edge failure analysis of laminated composite plate under in-plane tension

The project aims to study the free edge stress distributions response of a laminated composite subjected to an in-plane tension using a numerical finite element analysis software package, ANSYS. A systematic modelling approach was derived, in order to increase the confidence level of the numerical r...

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Bibliographic Details
Main Author: Lim, Tiong Hwa.
Other Authors: Chai, Gin Boay
Format: Thesis
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/6034
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author Lim, Tiong Hwa.
author2 Chai, Gin Boay
author_facet Chai, Gin Boay
Lim, Tiong Hwa.
author_sort Lim, Tiong Hwa.
collection NTU
description The project aims to study the free edge stress distributions response of a laminated composite subjected to an in-plane tension using a numerical finite element analysis software package, ANSYS. A systematic modelling approach was derived, in order to increase the confidence level of the numerical results obtained. A sensitivity study of stress distributions at the free edge zone affected by the mesh refinement was done. Through this study, an optimum mesh density was obtained by the study of the resultant stress convergent plots. Two different modelling techniques are explored, namely, using a full shell to sub-solid and a full solid to sub-solid. The results obtained suggested that there is only a subtle difference between both solutions. Finally, verification of the numerical results with the works of other researchers was performed; a good close matching among the results was observed.
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spelling ntu-10356/60342023-03-11T17:25:03Z Free edge failure analysis of laminated composite plate under in-plane tension Lim, Tiong Hwa. Chai, Gin Boay School of Mechanical and Production Engineering DRNTU::Engineering::Materials::Composite materials The project aims to study the free edge stress distributions response of a laminated composite subjected to an in-plane tension using a numerical finite element analysis software package, ANSYS. A systematic modelling approach was derived, in order to increase the confidence level of the numerical results obtained. A sensitivity study of stress distributions at the free edge zone affected by the mesh refinement was done. Through this study, an optimum mesh density was obtained by the study of the resultant stress convergent plots. Two different modelling techniques are explored, namely, using a full shell to sub-solid and a full solid to sub-solid. The results obtained suggested that there is only a subtle difference between both solutions. Finally, verification of the numerical results with the works of other researchers was performed; a good close matching among the results was observed. Master of Science (Mechanics & Processing of Materials) 2008-09-17T11:05:12Z 2008-09-17T11:05:12Z 2000 2000 Thesis http://hdl.handle.net/10356/6034 Nanyang Technological University application/pdf
spellingShingle DRNTU::Engineering::Materials::Composite materials
Lim, Tiong Hwa.
Free edge failure analysis of laminated composite plate under in-plane tension
title Free edge failure analysis of laminated composite plate under in-plane tension
title_full Free edge failure analysis of laminated composite plate under in-plane tension
title_fullStr Free edge failure analysis of laminated composite plate under in-plane tension
title_full_unstemmed Free edge failure analysis of laminated composite plate under in-plane tension
title_short Free edge failure analysis of laminated composite plate under in-plane tension
title_sort free edge failure analysis of laminated composite plate under in plane tension
topic DRNTU::Engineering::Materials::Composite materials
url http://hdl.handle.net/10356/6034
work_keys_str_mv AT limtionghwa freeedgefailureanalysisoflaminatedcompositeplateunderinplanetension