Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.

Fibre metal laminates (FMLs) are a family of hybrid materials currently being considered for use in airframe structural applications. Post-impact fatigue strength tests were carried out on kenaf short fibre polypropylene aluminum laminates on three different energy level. Three type of kenaf short f...

Full description

Saved in:

Bibliographic Details
Main Author:	Abdul Mubin, Abdul Adzim
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Mechanics applied to machinery Dynamics
Online Access:	https://ir.uitm.edu.my/id/eprint/31090/2/31090.pdf
Tags:	Add Tag No Tags, Be the first to tag this record!

id	my-uitm-ir.31090
record_format	uketd_dc
spelling	my-uitm-ir.310902023-12-27T07:45:32Z Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin. 2009-05 Abdul Mubin, Abdul Adzim Mechanics applied to machinery. Dynamics Fibre metal laminates (FMLs) are a family of hybrid materials currently being considered for use in airframe structural applications. Post-impact fatigue strength tests were carried out on kenaf short fibre polypropylene aluminum laminates on three different energy level. Three type of kenaf short fibre polypropylene composite are prepared consist of three different weight ratio. The ratios of the composite prepared are 15% wt kenaf fibre and 85% wt PP (Composite A), 20%wt kenaf fibre and 80% wt PP (Composite B) and 25%wt kenaf fibre and 75% wt PP (Composite C). The composites specimens are then subjected to tensile test to see which ratio of specimen hold the best tensile strength properties. The results revealed that Composite C holds the best tensile strength by 24% than Composite A and 16% than Composite B. Then Composite C is chosen for fabrication of the FML. The specimens then are impacted at three different energy levels using post impact fixture. The energy levels that are used during this experiment are 0.55 J, 0.94 J and 2.23 J. The impacted specimens are then subjected to tensile and fatigue test until failure to determine the residual strength of the FML. The results revealed that even low energy impact could seriously impair the tensile properties. Low velocity impact also reduced the fatigue lives of the FML and this reduction could be related to the degradation in tensile strength. 2009-05 Thesis https://ir.uitm.edu.my/id/eprint/31090/ https://ir.uitm.edu.my/id/eprint/31090/2/31090.pdf text en public degree Universiti Teknologi MARA Shah Alam Faculty of Mechanical Engineering Md Taib, Yakub
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Md Taib, Yakub
topic	Mechanics applied to machinery Dynamics
spellingShingle	Mechanics applied to machinery Dynamics Abdul Mubin, Abdul Adzim Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
description	Fibre metal laminates (FMLs) are a family of hybrid materials currently being considered for use in airframe structural applications. Post-impact fatigue strength tests were carried out on kenaf short fibre polypropylene aluminum laminates on three different energy level. Three type of kenaf short fibre polypropylene composite are prepared consist of three different weight ratio. The ratios of the composite prepared are 15% wt kenaf fibre and 85% wt PP (Composite A), 20%wt kenaf fibre and 80% wt PP (Composite B) and 25%wt kenaf fibre and 75% wt PP (Composite C). The composites specimens are then subjected to tensile test to see which ratio of specimen hold the best tensile strength properties. The results revealed that Composite C holds the best tensile strength by 24% than Composite A and 16% than Composite B. Then Composite C is chosen for fabrication of the FML. The specimens then are impacted at three different energy levels using post impact fixture. The energy levels that are used during this experiment are 0.55 J, 0.94 J and 2.23 J. The impacted specimens are then subjected to tensile and fatigue test until failure to determine the residual strength of the FML. The results revealed that even low energy impact could seriously impair the tensile properties. Low velocity impact also reduced the fatigue lives of the FML and this reduction could be related to the degradation in tensile strength.
format	Thesis
qualification_level	Bachelor degree
author	Abdul Mubin, Abdul Adzim
author_facet	Abdul Mubin, Abdul Adzim
author_sort	Abdul Mubin, Abdul Adzim
title	Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
title_short	Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
title_full	Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
title_fullStr	Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
title_full_unstemmed	Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.
title_sort	post impact fatigue of fibre metal laminate (fml) / abdul adzim abdul mubin.
granting_institution	Universiti Teknologi MARA Shah Alam
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/31090/2/31090.pdf
_version_	1794191815667089408

Post impact fatigue of fibre metal laminate (FML) / Abdul Adzim Abdul Mubin.

Similar Items