Damage Mechanisms of Inconel738LC under creep-fatigue loading conditions

机译：蠕变疲劳载荷条件下Inconel738LC的损伤机理

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In order to investigate creep-fatigue life characgterisitc of Incone1738LC, fatigue and creep-fatigue tests were carried out at 850 degree. Significant life reduction to 30

机译：为了研究Incone1738LC的蠕变疲劳寿命特性，在850度下进行了疲劳和蠕变疲劳测试。寿命大幅减少至30

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来源
《Proceedings of Third Sino-Japan bilateral symposium on high temperature strength of materials》|1998年|p.162-169|共8页
会议地点 Nanjing(CN)
作者
M.Yamamoto; T.Ogata;
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原文格式 PDF
正文语种 eng
中图分类一般工业技术;
关键词
superalloy; creep-fatigue; grain boundry sliding;

机译：高温合金蠕变疲劳晶界滑动;

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Damage Mechanisms of Inconel738LC under creep-fatigue loading conditions

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