Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load
This project involves the study of the effects of coupling in Steel/Aluminium laminate subjected to tension and bending load. The engineering simulation and design software, ANSYS, was used to aid the simulation and analysis of the laminate under load. Finite element modelling was applied to obtain...
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2020
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sg-ntu-dr.10356-1410332023-03-04T19:30:12Z Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load Goh, Pei Yi Chai Gin Boay School of Mechanical and Aerospace Engineering MGBCHAI@ntu.edu.sg Engineering::Aeronautical engineering::Materials of construction This project involves the study of the effects of coupling in Steel/Aluminium laminate subjected to tension and bending load. The engineering simulation and design software, ANSYS, was used to aid the simulation and analysis of the laminate under load. Finite element modelling was applied to obtain the results in this report. To carry out the simulation, a cantilevered laminate plate of thickness 2.72mm, width 200mm and length 500m is loaded at the tip. This load was varied from 5N to 25N. The plies within the laminate is increased from 2 to 8 with the thickness kept constant throughout. The Aluminium and Steel laminate produced a coupling effect presented in this report. It is found that the stiffness increases with the number of plies in the laminate. Bachelor of Engineering (Aerospace Engineering) 2020-06-03T08:07:49Z 2020-06-03T08:07:49Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/141033 en application/pdf Nanyang Technological University |
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Engineering::Aeronautical engineering::Materials of construction Goh, Pei Yi Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
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This project involves the study of the effects of coupling in Steel/Aluminium laminate subjected to tension and bending load. The engineering simulation and design software, ANSYS, was used to aid the simulation and analysis of the laminate under load. Finite element modelling was applied to obtain the results in this report. To carry out the simulation, a cantilevered laminate plate of thickness 2.72mm, width 200mm and length 500m is loaded at the tip. This load was varied from 5N to 25N. The plies within the laminate is increased from 2 to 8 with the thickness kept constant throughout. The Aluminium and Steel laminate produced a coupling effect presented in this report. It is found that the stiffness increases with the number of plies in the laminate. |
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Chai Gin Boay |
author_facet |
Chai Gin Boay Goh, Pei Yi |
format |
Final Year Project |
author |
Goh, Pei Yi |
author_sort |
Goh, Pei Yi |
title |
Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
title_short |
Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
title_full |
Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
title_fullStr |
Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
title_full_unstemmed |
Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load |
title_sort |
analysis of the effect of coupling in steel/aluminium laminate under bending and tension load |
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Nanyang Technological University |
publishDate |
2020 |
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https://hdl.handle.net/10356/141033 |
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1759857890660712448 |