Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza

This research study on the mechanical and physical properties of low-velocity damage keratin filled/glass fiber sandwiched composite. In this research, fiber filler used is the pulverised chicken feather which varies at 10%, 20%, 30%, 40% and 50% by weight. The chicken feather composite then laminat...

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Main Author: Abdul Hamid Ridza, Khairunnisa Liyana
Format: Thesis
Language:English
Published: 2016
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Online Access:https://ir.uitm.edu.my/id/eprint/101852/1/101852.pdf
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spelling my-uitm-ir.1018522024-11-12T07:57:34Z Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza 2016 Abdul Hamid Ridza, Khairunnisa Liyana Composite materials. This research study on the mechanical and physical properties of low-velocity damage keratin filled/glass fiber sandwiched composite. In this research, fiber filler used is the pulverised chicken feather which varies at 10%, 20%, 30%, 40% and 50% by weight. The chicken feather composite then laminates with woven glass fiber at two types of laminate arrangement; single side laminates and both side laminates. The composite samples were cut to a required dimension for the mechanical and physical test. Optimum low-velocity impact energy was determined by applying 5% of maximum impact energy, damages toward the sample may not be seen by naked eyes. Morphology of low-velocity impacted sample was observed at the dented areas using metallurgical microscope. Both impacted and non-impacted samples were examine for its tensile properties. The impacted sample have lower tensile strength than the non-impacted sample. The presence of crack and void at dented area cause the impacted sample prone to failure at low tensile stress. As the chicken feather loading increase for both impacted and non-impacted, there are decreasing pattern of tensile strength. The incorporation of 10% to 30% chicken feather in the epoxy resulting several fiber pull out. At higher loading of 40% to 50% chicken feather, there are restriction for epoxy to penetrate between the chicken feathers. Thus failed to enhance load transfer and results in fiber fracture. Apart of the tensile properties, density and water absorption were also investigated. The water absorption was relying on attraction of water molecule to feather fiber. The more keratin filler incorporated in sample, the higher water being absorbed. 2016 Thesis https://ir.uitm.edu.my/id/eprint/101852/ https://ir.uitm.edu.my/id/eprint/101852/1/101852.pdf text en public masters Universiti Teknologi MARA (UiTM) Faculty of Applied Science
institution Universiti Teknologi MARA
collection UiTM Institutional Repository
language English
topic Composite materials.
spellingShingle Composite materials.
Abdul Hamid Ridza, Khairunnisa Liyana
Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
description This research study on the mechanical and physical properties of low-velocity damage keratin filled/glass fiber sandwiched composite. In this research, fiber filler used is the pulverised chicken feather which varies at 10%, 20%, 30%, 40% and 50% by weight. The chicken feather composite then laminates with woven glass fiber at two types of laminate arrangement; single side laminates and both side laminates. The composite samples were cut to a required dimension for the mechanical and physical test. Optimum low-velocity impact energy was determined by applying 5% of maximum impact energy, damages toward the sample may not be seen by naked eyes. Morphology of low-velocity impacted sample was observed at the dented areas using metallurgical microscope. Both impacted and non-impacted samples were examine for its tensile properties. The impacted sample have lower tensile strength than the non-impacted sample. The presence of crack and void at dented area cause the impacted sample prone to failure at low tensile stress. As the chicken feather loading increase for both impacted and non-impacted, there are decreasing pattern of tensile strength. The incorporation of 10% to 30% chicken feather in the epoxy resulting several fiber pull out. At higher loading of 40% to 50% chicken feather, there are restriction for epoxy to penetrate between the chicken feathers. Thus failed to enhance load transfer and results in fiber fracture. Apart of the tensile properties, density and water absorption were also investigated. The water absorption was relying on attraction of water molecule to feather fiber. The more keratin filler incorporated in sample, the higher water being absorbed.
format Thesis
qualification_level Master's degree
author Abdul Hamid Ridza, Khairunnisa Liyana
author_facet Abdul Hamid Ridza, Khairunnisa Liyana
author_sort Abdul Hamid Ridza, Khairunnisa Liyana
title Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
title_short Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
title_full Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
title_fullStr Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
title_full_unstemmed Effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / Khairunnisa Liyana Abdul Hamid Ridza
title_sort effect of low-velocity impact damage to the mechanical properties of glass fiber/keratin filler sandwiched thermosets composite / khairunnisa liyana abdul hamid ridza
granting_institution Universiti Teknologi MARA (UiTM)
granting_department Faculty of Applied Science
publishDate 2016
url https://ir.uitm.edu.my/id/eprint/101852/1/101852.pdf
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