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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/100112

    Authors: Chen, Pu-Woei;Chang, Shu-Han;Siao, Jyun-Yuan
    Contributors: 淡江大學航空太空工程學系
    Keywords: damage tolerance;crack propagation;finite element analysis;light aircraft
    Date: 2013-09-01
    Issue Date: 2015-01-28 11:07:50 (UTC+8)
    Publisher: Canada: Canadian Society for Mechanical Engineering
    Abstract: 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.
    Relation: Transactions of the Canadian Society for Mechanical Engineering 37(4), pp.1147-1159
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

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