Low velocity impact sandwich structure bamboo for aerospace applications
Abundant sources of bamboo in Malaysia, if fully utilized, can increase its commercial value especially in developing greener composites. In this study, material characterizations on bamboo based composites, from Malaysian species of Bambusa vulgaris, were carried out by aiming on the low velo...
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my-upm-ir.756952019-11-20T02:51:37Z Low velocity impact sandwich structure bamboo for aerospace applications 2018-03 Md. Shah, Ain Umara Abundant sources of bamboo in Malaysia, if fully utilized, can increase its commercial value especially in developing greener composites. In this study, material characterizations on bamboo based composites, from Malaysian species of Bambusa vulgaris, were carried out by aiming on the low velocity impact properties. Bamboo powder, as the raw material in composites, was selfprocessed through a combination of manual and machining methods. Four different loadings of bamboo powder, which ranged from 500μm to 1mm in size, consisting of 0%, 10%, 20%, and 30% by weight were applied in the preparation of the composites. Woven glass fibre type E600, embedded at the outermost top and bottom layer of composites, was used as the main reinforcement with epoxy as the polymer matrix. Sandwich structured composites were fabricated through a combination of manual hand lay-up and compression moulding techniques. From the tensile testing and scanning electron microscopy images, poor bamboo-epoxy interfacial bonding lowered the strength of the composites as the fibre loading increased. However, the highest percentage of 30% loading suggested good stress transfer in composites through observation of the peak of the Tan δ curve through dynamic mechanical analysis. For both thermal degradation and water absorption properties, the addition of bamboo fibres lowers the thermal stability and enhances the water absorption respectively, which are the drawbacks of using natural fibres. Inconsistent damage propagations were observed on the non-hybrid bamboo composites after low velocity impact due to short size bamboo fibres aligned in random orientation within the epoxy matrix. However, the impact resistance increased as the bamboo fibre loading increased. The inclusion of woven glass fibres at the top and bottom layer of the composites significantly improved the impact resistance as these layers slowed down the penetration of the impactor, thus reducing the severity of the damages. Generally, the newly developed sandwich structured bamboo filled glass-epoxy hybrid composites have potential to be used in aerospace applications with low velocity impact properties. Aerospace engineering Velocity modulation 2018-03 Thesis http://psasir.upm.edu.my/id/eprint/75695/ http://psasir.upm.edu.my/id/eprint/75695/1/FK%202018%20140%20-%20IR.pdf text en public doctoral Universiti Putra Malaysia Aerospace engineering Velocity modulation |
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Universiti Putra Malaysia |
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English |
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Aerospace engineering Velocity modulation |
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Aerospace engineering Velocity modulation Md. Shah, Ain Umara Low velocity impact sandwich structure bamboo for aerospace applications |
| description |
Abundant sources of bamboo in Malaysia, if fully utilized, can increase its
commercial value especially in developing greener composites. In this study,
material characterizations on bamboo based composites, from Malaysian
species of Bambusa vulgaris, were carried out by aiming on the low velocity
impact properties. Bamboo powder, as the raw material in composites, was selfprocessed
through a combination of manual and machining methods. Four
different loadings of bamboo powder, which ranged from 500μm to 1mm in size,
consisting of 0%, 10%, 20%, and 30% by weight were applied in the preparation
of the composites. Woven glass fibre type E600, embedded at the outermost top
and bottom layer of composites, was used as the main reinforcement with epoxy
as the polymer matrix. Sandwich structured composites were fabricated through
a combination of manual hand lay-up and compression moulding techniques.
From the tensile testing and scanning electron microscopy images, poor
bamboo-epoxy interfacial bonding lowered the strength of the composites as the
fibre loading increased. However, the highest percentage of 30% loading
suggested good stress transfer in composites through observation of the peak of
the Tan δ curve through dynamic mechanical analysis. For both thermal
degradation and water absorption properties, the addition of bamboo fibres
lowers the thermal stability and enhances the water absorption respectively,
which are the drawbacks of using natural fibres. Inconsistent damage
propagations were observed on the non-hybrid bamboo composites after low
velocity impact due to short size bamboo fibres aligned in random orientation
within the epoxy matrix. However, the impact resistance increased as the
bamboo fibre loading increased. The inclusion of woven glass fibres at the top
and bottom layer of the composites significantly improved the impact resistance
as these layers slowed down the penetration of the impactor, thus reducing the
severity of the damages. Generally, the newly developed sandwich structured
bamboo filled glass-epoxy hybrid composites have potential to be used in
aerospace applications with low velocity impact properties. |
| format |
Thesis |
| qualification_level |
Doctorate |
| author |
Md. Shah, Ain Umara |
| author_facet |
Md. Shah, Ain Umara |
| author_sort |
Md. Shah, Ain Umara |
| title |
Low velocity impact sandwich structure bamboo for aerospace applications |
| title_short |
Low velocity impact sandwich structure bamboo for aerospace applications |
| title_full |
Low velocity impact sandwich structure bamboo for aerospace applications |
| title_fullStr |
Low velocity impact sandwich structure bamboo for aerospace applications |
| title_full_unstemmed |
Low velocity impact sandwich structure bamboo for aerospace applications |
| title_sort |
low velocity impact sandwich structure bamboo for aerospace applications |
| granting_institution |
Universiti Putra Malaysia |
| publishDate |
2018 |
| url |
http://psasir.upm.edu.my/id/eprint/75695/1/FK%202018%20140%20-%20IR.pdf |
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