Please use this identifier to cite or link to this item:
https://hdl.handle.net/10356/141033
Title: | Analysis of the effect of coupling in Steel/Aluminium laminate under bending and tension load | Authors: | Goh, Pei Yi | Keywords: | Engineering::Aeronautical engineering::Materials of construction | Issue Date: | 2020 | Publisher: | Nanyang Technological University | Abstract: | 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. | URI: | https://hdl.handle.net/10356/141033 | Schools: | School of Mechanical and Aerospace Engineering | Fulltext Permission: | restricted | Fulltext Availability: | With Fulltext |
Appears in Collections: | MAE Student Reports (FYP/IA/PA/PI) |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Goh Pei Yi FYP.pdf Restricted Access | 1.87 MB | Adobe PDF | View/Open |
Page view(s)
356
Updated on May 7, 2025
Download(s)
20
Updated on May 7, 2025
Google ScholarTM
Check
Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.