Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications

The usage of natural fibres as a reinforcement in material composites has increased over time. This utilization had been applied widely in several regions of the world and has already reached maturity in terms of technology, infrastructure and cost competitiveness. Aerospace industries were looking...

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Main Author: Ismail, Muhammad Faizzuddin
Format: Thesis
Language:English
Published: 2018
Subjects:
Online Access:http://psasir.upm.edu.my/id/eprint/77755/1/FK%202019%2053%20ir.pdf
http://psasir.upm.edu.my/id/eprint/77755/
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Institution: Universiti Putra Malaysia
Language: English
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spelling my.upm.eprints.777552022-01-24T03:09:42Z http://psasir.upm.edu.my/id/eprint/77755/ Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications Ismail, Muhammad Faizzuddin The usage of natural fibres as a reinforcement in material composites has increased over time. This utilization had been applied widely in several regions of the world and has already reached maturity in terms of technology, infrastructure and cost competitiveness. Aerospace industries were looking forwards on fully utilized their structural components by using composites material towards environmentally friendly solutions. The application of hybrid composites can be utilized by reducing the usage of synthetic fibre and replacing them with natural fibre. Nonetheless, the applications of composites in aircraft’s structure is tends to develop, especially the use of hybrid composites for fuselage which has many conflicting requirements. Several issues are highlighted in this research such as the selection of natural fibre that suits the usage in aerospace structural applications and the most suitable weight percentage combinations of individual fibre in hybrid composites that approaching the original constituents. Hence, the objectives of this research can be summarised as follows: the mechanical properties of a hybrid composite of glass/ kenaf fibre were investigated, especially with regards to tensile strength and low velocity impact (LVIT) resistance. A non-destructive test (NDT) was conducted by using dye penetrant to inspect the damages after impact where those areas were measured and analysed. The compression after impact (CAI) test was also performed on the impacted hybrid composite samples to analyse further the damage progression of the sample from the compressive aspect. It was found that, through mechanical analysis, the hybrid composite with the combination of 75% weight percentage of glass fibre and 25% weight percentage of kenaf fibre had the best tensile properties that approaching the tensile strength of 100% glass fibre. Furthermore, the best selected sample may experience LVIT impact forces up to 40 Joule. The higher impact force had led to larger damage and dents areas. CAI tests were carried out resulting in the decreases of the compression force exerted to the impacted damaged of the 40 Joule’s sample. 2018-10 Thesis NonPeerReviewed text en http://psasir.upm.edu.my/id/eprint/77755/1/FK%202019%2053%20ir.pdf Ismail, Muhammad Faizzuddin (2018) Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications. Masters thesis, Universiti Putra Malaysia. Aerospace engineering Velocity modulation Kenaf
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
topic Aerospace engineering
Velocity modulation
Kenaf
spellingShingle Aerospace engineering
Velocity modulation
Kenaf
Ismail, Muhammad Faizzuddin
Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
description The usage of natural fibres as a reinforcement in material composites has increased over time. This utilization had been applied widely in several regions of the world and has already reached maturity in terms of technology, infrastructure and cost competitiveness. Aerospace industries were looking forwards on fully utilized their structural components by using composites material towards environmentally friendly solutions. The application of hybrid composites can be utilized by reducing the usage of synthetic fibre and replacing them with natural fibre. Nonetheless, the applications of composites in aircraft’s structure is tends to develop, especially the use of hybrid composites for fuselage which has many conflicting requirements. Several issues are highlighted in this research such as the selection of natural fibre that suits the usage in aerospace structural applications and the most suitable weight percentage combinations of individual fibre in hybrid composites that approaching the original constituents. Hence, the objectives of this research can be summarised as follows: the mechanical properties of a hybrid composite of glass/ kenaf fibre were investigated, especially with regards to tensile strength and low velocity impact (LVIT) resistance. A non-destructive test (NDT) was conducted by using dye penetrant to inspect the damages after impact where those areas were measured and analysed. The compression after impact (CAI) test was also performed on the impacted hybrid composite samples to analyse further the damage progression of the sample from the compressive aspect. It was found that, through mechanical analysis, the hybrid composite with the combination of 75% weight percentage of glass fibre and 25% weight percentage of kenaf fibre had the best tensile properties that approaching the tensile strength of 100% glass fibre. Furthermore, the best selected sample may experience LVIT impact forces up to 40 Joule. The higher impact force had led to larger damage and dents areas. CAI tests were carried out resulting in the decreases of the compression force exerted to the impacted damaged of the 40 Joule’s sample.
format Thesis
author Ismail, Muhammad Faizzuddin
author_facet Ismail, Muhammad Faizzuddin
author_sort Ismail, Muhammad Faizzuddin
title Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
title_short Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
title_full Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
title_fullStr Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
title_full_unstemmed Low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
title_sort low velocity impact analysis of glass/kenaf hybrid composites for aerospace structural applications
publishDate 2018
url http://psasir.upm.edu.my/id/eprint/77755/1/FK%202019%2053%20ir.pdf
http://psasir.upm.edu.my/id/eprint/77755/
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