Building of composite system for Wing using Prepreg
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Universiti Malaysia Perlis
2008
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my.unimap-32682008-11-17T07:17:42Z Building of composite system for Wing using Prepreg Siti Noorkhartina Ishak Mohd Nasir Zainal Arif, Prof. Dr. (Advisor) Composites Composite materials Polymers Fibers Fibrous composites Access is limited to UniMAP community. The effect of fibre reinforcement and resin content on moisture uptake in composite laminate was investigated. Three materials using identical epoxy resin systems but different reinforcements glass, kevlar and carbon fibers and immersed in metyl ethyl keton( MEK ) solven were examined. Samples were characterized by DSC in terms of percent of resin in prepreg. Mechanical and thermal properties including tensile modulus, tensile strength, and glass transition temperature were measured. Expired graphite show the highest modulus than good graphite. Modulus value of expired graphite is 56.96 GPa while good prepreg only 32.503 GPa. Young’s modulus whether good or expired fiberglass show the lowest value that is in range 1.45 GPa to 2.45 GPa. Results clearly show the contribution of the fiber reinforcement as well as resin content percentage rate and mechanical property changes. For resin content all sample show the the percentage of volume fraction in range. 2008-11-17T07:17:42Z 2008-11-17T07:17:42Z 2008-04 Learning Object http://hdl.handle.net/123456789/3268 en Universiti Malaysia Perlis School of Materials Engineering |
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Composites Composite materials Polymers Fibers Fibrous composites |
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Composites Composite materials Polymers Fibers Fibrous composites Siti Noorkhartina Ishak Building of composite system for Wing using Prepreg |
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Mohd Nasir Zainal Arif, Prof. Dr. (Advisor) |
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Mohd Nasir Zainal Arif, Prof. Dr. (Advisor) Siti Noorkhartina Ishak |
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Siti Noorkhartina Ishak |
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Siti Noorkhartina Ishak |
title |
Building of composite system for Wing using Prepreg |
title_short |
Building of composite system for Wing using Prepreg |
title_full |
Building of composite system for Wing using Prepreg |
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Building of composite system for Wing using Prepreg |
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Building of composite system for Wing using Prepreg |
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building of composite system for wing using prepreg |
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Universiti Malaysia Perlis |
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2008 |
url |
http://dspace.unimap.edu.my/xmlui/handle/123456789/3268 |
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1643787810258288640 |