On the fatigue crack growth analysis of spliced aircraft wing panels under sequential axial and shear loads

标题
On the fatigue crack growth analysis of spliced aircraft wing panels under sequential axial and shear loads
作者
关键词
-
出版物
ENGINEERING FRACTURE MECHANICS
Volume 123, Issue -, Pages 116-125
出版商
Elsevier BV
发表日期
2014-04-03
DOI
10.1016/j.engfracmech.2014.03.018

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