A new multiaxial fatigue life prediction model for aircraft aluminum alloy

标题
A new multiaxial fatigue life prediction model for aircraft aluminum alloy
作者
关键词
Multiaxial fatigue life prediction, Aircraft aluminum alloy, Critical plane approach, Additional hardening, Non-proportional loading
出版物
INTERNATIONAL JOURNAL OF FATIGUE
Volume 143, Issue -, Pages 105993
出版商
Elsevier BV
发表日期
2020-10-16
DOI
10.1016/j.ijfatigue.2020.105993

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