The Orientation and Strength of Riveted Joints on Aircraft Panel

Please use this identifier to cite or link to this item: http://hdl.handle.net/123456789/10883

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DC Field	Value	Language
dc.contributor.author	Muhammad Ikhwan Bin Khairuddin	-
dc.date.accessioned	2015-09-14T19:17:30Z	-
dc.date.available	2015-09-14T19:17:30Z	-
dc.date.issued	2015-09-15	-
dc.identifier.uri	http://localhost/xmlui/handle/123456789/10883	-
dc.description	Bachelor of Engineering Technology December 2014	en_US
dc.description.abstract	The purpose of this project is to compare the strength between the riveted joints and which rivet has a better joint strength. In order to achieve this, sheet metal with aircraft specification is needed and must be riveted with 2 types of riveted joints. 2 type of rivet are used to achieve different results. The test of the strength will be tested using Universal Testing Machine (UTM).	en_US
dc.language.iso	en_US	en_US
dc.title	The Orientation and Strength of Riveted Joints on Aircraft Panel	en_US
Appears in Collections:	Final Year Project - UniKL MIAT

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