淡江大學機構典藏:Item 987654321/100112
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    题名: AN ANALYSIS OF THE DAMAGE TOLERANCE OF LIGHT AIRCRAFT LANDING GEAR
    作者: Chen, Pu-Woei;Chang, Shu-Han;Siao, Jyun-Yuan
    贡献者: 淡江大學航空太空工程學系
    关键词: damage tolerance;crack propagation;finite element analysis;light aircraft
    日期: 2013-09-01
    上传时间: 2015-01-28 11:07:50 (UTC+8)
    出版者: Canada: Canadian Society for Mechanical Engineering
    摘要: This study uses the finite element software, FRANC2D, and the life-time analysis software, AFGROW, to perform simulation analyses of the damage tolerance of the landing gear of light aviation vehicles. This study explores the effect that the initial crack positions and different materials have on the life cycle of landing gear under long-term loads. This study also compares the relationship between stress intensity factors and crack growth for four types of aluminum alloys, titanium alloy and alloy steel. The relationship between residual strength and life cycle, in the presence of existing cracks, is also investigated.
    關聯: Transactions of the Canadian Society for Mechanical Engineering 37(4), pp.1147-1159
    显示于类别:[航空太空工程學系暨研究所] 期刊論文

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