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http://hdl.handle.net/123456789/25094
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DC Field | Value | Language |
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dc.contributor.author | Sharifah Fathin Adlina Syed Abdullah | - |
dc.contributor.author | Nurul Zuhairah Mahmud Zuhudi | - |
dc.contributor.author | Khairul Dahri Mohd Aris | - |
dc.contributor.author | Mohd Nazrul Roslan | - |
dc.contributor.author | Mohamad Dali Isa | - |
dc.date.accessioned | 2021-08-15T10:27:22Z | - |
dc.date.available | 2021-08-15T10:27:22Z | - |
dc.date.issued | 2019-11-20 | - |
dc.identifier.citation | Sharifah Fathin Adlina Syed Abdullah,Nurul Zuhairah Mahmud Zuhudi,Khairul Dahri Mohd Aris, Mohd Nazrul Roslan, Mohamad Dali Isa, Physical and mechanical characterization of kenaf fiber filament wound composite produced using vacuum-bagging and heat-shrink tube method, Lecture Notes in Mechanical Engineering, 2020, Pages 519-527, 2nd International Conference of Aerospace and Mechanical Engineering, AeroMech 2019; Seberang Perai; Malaysia; 20 November 2019 through 21 November 2019; Code 241099, DOI: 10.1007/978-981-15-4756-0_46 | en_US |
dc.identifier.isbn | 978-981154755-3 | - |
dc.identifier.issn | 21954356 | - |
dc.identifier.uri | http://hdl.handle.net/123456789/25094 | - |
dc.description | UniKL MIAT | en_US |
dc.description.abstract | Most natural fiber reinforcements in the industry are based on random discontinuous fibers. This study aims to demonstrate the potential of continuous natural fiber-reinforced composites in structural applications. Kenaf-cotton yarn composites have been manufactured by dry filament-winding process with winding angle that varies from 50 to 80° and wet lay-up assisted by two methods, i.e. vacuum-bagging and heat-shrink tube. A hoop tensile strength test was conducted and winding angle of 80o was found to give the highest tensile strength of approximately 49.3 MPa. Heat-shrink tube method improved composites performance by 36%. © Springer Nature Singapore Pte Ltd 2020. | en_US |
dc.language.iso | en | en_US |
dc.publisher | Springer | en_US |
dc.subject | Filament winding | en_US |
dc.subject | Filament wound | en_US |
dc.subject | Kenaf | en_US |
dc.subject | Natural fiber composites | en_US |
dc.subject | Tubular | en_US |
dc.title | Physical and Mechanical Characterization of Kenaf Fiber Filament Wound Composite Produced Using Vacuum-Bagging and Heat-Shrink Tube Method | en_US |
dc.type | Working Paper | en_US |
dc.conference.name | 2nd International Conference of Aerospace and Mechanical Engineering, AeroMech 2019 | en_US |
dc.conference.year | 2019 | en_US |
Appears in Collections: | Conference Paper |
Files in This Item:
File | Description | Size | Format | |
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Abstract physical & mech.docx | 11.9 kB | Microsoft Word XML | View/Open Request a copy |
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