Static tensile and fatigue and testing of aluminium plate with holes and cracks

In an aircraft structure, fatigue failures usually started from the initiation and propagation of cracks from notches or defects. For example, an aircraft usually has a lot of rivet holes. High stress concentrations are usually found on these holes and these are the likely places for the development...

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主要作者: Yeap, Shi Hong
其他作者: Chai Gin Boay
格式: Final Year Project
語言:English
出版: 2011
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在線閱讀:http://hdl.handle.net/10356/46165
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機構: Nanyang Technological University
語言: English