Crack growth and delamination behaviour in advanced Al-Li alloy laminate under constant amplitude fatigue loading

被引：0
|
作者：
Beijing Institute of Aeronautical Materials, Beijing [1 ]
100095, China
不详 [2 ]
机构：
来源：
Mater. Res. Innov. | / 685-689期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
D O I：
10.1179/1432891715Z.0000000001777
中图分类号：
学科分类号：
摘要：
Fibers - Failure (mechanical) - Fatigue crack propagation - Aluminum alloys - Delamination - Lithium alloys
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页码：685 / 689
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