Bending of fibre-metal sandwich beams

A sandwich beam is a special composite structure that is made up by bonding two thin but stiff face sheets to a lightweight but thick core. This unique design gives rise to a lightweight structure with high bending stiffness. The application of such structures are very useful in aerospace industry w...

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Main Author: Guo, Hanwei
Other Authors: Chai Gin Boay
Format: Final Year Project
Language:English
Published: 2016
Subjects:
Online Access:http://hdl.handle.net/10356/68497
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-684972023-03-04T18:19:09Z Bending of fibre-metal sandwich beams Guo, Hanwei Chai Gin Boay School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Materials of construction A sandwich beam is a special composite structure that is made up by bonding two thin but stiff face sheets to a lightweight but thick core. This unique design gives rise to a lightweight structure with high bending stiffness. The application of such structures are very useful in aerospace industry where weight saving is very important. The objective of this project is to study structural response of sandwich beams, made up of fibre-metal face sheets with honeycomb core, under bending loads. Sandwich beams with Aluminium 2024-T3 face sheets, FRP face sheets and Fibre Metal Laminate (FML) face sheets were fabricated. They were subjected to three point bending tests to evaluate their failure modes and compare their flexural properties. In addition, a comparison was also done on FML beams with different span lengths to investigate the effects of span/thickness ratio. Based on the experimental results, core shear was the most common dominant failure mode in the all sandwich beams. FML beams had more globalized damage than carbon fibre beams which had more localized damage. On top of that, skin wrinkling was only observed in aluminium beams, but not in two other beams. The data collected also revealed that maximum loads for FML beams and carbon fibres beams are comparable, however FMLs beams were able to withstand higher post-failure load and absorb more energy. A comparison between FML beams with different span length/thickness shows that the maximum loads for the beams were independent of the span length/thickness ratio. Beams with smaller length/thickness ratio were observed to be more resistant to bending and had more localized damage than beams with higher span/thickness ratio. Bachelor of Engineering (Aerospace Engineering) 2016-05-26T05:00:09Z 2016-05-26T05:00:09Z 2016 Final Year Project (FYP) http://hdl.handle.net/10356/68497 en Nanyang Technological University 79 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Materials of construction
spellingShingle DRNTU::Engineering::Aeronautical engineering::Materials of construction
Guo, Hanwei
Bending of fibre-metal sandwich beams
description A sandwich beam is a special composite structure that is made up by bonding two thin but stiff face sheets to a lightweight but thick core. This unique design gives rise to a lightweight structure with high bending stiffness. The application of such structures are very useful in aerospace industry where weight saving is very important. The objective of this project is to study structural response of sandwich beams, made up of fibre-metal face sheets with honeycomb core, under bending loads. Sandwich beams with Aluminium 2024-T3 face sheets, FRP face sheets and Fibre Metal Laminate (FML) face sheets were fabricated. They were subjected to three point bending tests to evaluate their failure modes and compare their flexural properties. In addition, a comparison was also done on FML beams with different span lengths to investigate the effects of span/thickness ratio. Based on the experimental results, core shear was the most common dominant failure mode in the all sandwich beams. FML beams had more globalized damage than carbon fibre beams which had more localized damage. On top of that, skin wrinkling was only observed in aluminium beams, but not in two other beams. The data collected also revealed that maximum loads for FML beams and carbon fibres beams are comparable, however FMLs beams were able to withstand higher post-failure load and absorb more energy. A comparison between FML beams with different span length/thickness shows that the maximum loads for the beams were independent of the span length/thickness ratio. Beams with smaller length/thickness ratio were observed to be more resistant to bending and had more localized damage than beams with higher span/thickness ratio.
author2 Chai Gin Boay
author_facet Chai Gin Boay
Guo, Hanwei
format Final Year Project
author Guo, Hanwei
author_sort Guo, Hanwei
title Bending of fibre-metal sandwich beams
title_short Bending of fibre-metal sandwich beams
title_full Bending of fibre-metal sandwich beams
title_fullStr Bending of fibre-metal sandwich beams
title_full_unstemmed Bending of fibre-metal sandwich beams
title_sort bending of fibre-metal sandwich beams
publishDate 2016
url http://hdl.handle.net/10356/68497
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