Please use this identifier to cite or link to this item: http://hdl.handle.net/123456789/25094
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dc.contributor.authorSharifah Fathin Adlina Syed Abdullah-
dc.contributor.authorNurul Zuhairah Mahmud Zuhudi-
dc.contributor.authorKhairul Dahri Mohd Aris-
dc.contributor.authorMohd Nazrul Roslan-
dc.contributor.authorMohamad Dali Isa-
dc.date.accessioned2021-08-15T10:27:22Z-
dc.date.available2021-08-15T10:27:22Z-
dc.date.issued2019-11-20-
dc.identifier.citationSharifah 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_46en_US
dc.identifier.isbn978-981154755-3-
dc.identifier.issn21954356-
dc.identifier.urihttp://hdl.handle.net/123456789/25094-
dc.descriptionUniKL MIATen_US
dc.description.abstractMost 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.isoenen_US
dc.publisherSpringeren_US
dc.subjectFilament windingen_US
dc.subjectFilament wounden_US
dc.subjectKenafen_US
dc.subjectNatural fiber compositesen_US
dc.subjectTubularen_US
dc.titlePhysical and Mechanical Characterization of Kenaf Fiber Filament Wound Composite Produced Using Vacuum-Bagging and Heat-Shrink Tube Methoden_US
dc.typeWorking Paperen_US
dc.conference.name2nd International Conference of Aerospace and Mechanical Engineering, AeroMech 2019en_US
dc.conference.year2019en_US
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