doi.org/10.1016/j.engfailanal.2020.104516
Other

XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug

..., Simon Sedmak
14
Engineering Failure Analysis4.40
Volume: 112, Pages: 104516 - 104516
Published: Mar 28, 2020
Paper Fields
Paper Details
Title
XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug
DOI
doi.org/10.1016/j.engfailanal.2020.104516
Published Date
Mar 28, 2020
Journal
Engineering Failure Analysis
Volume
112
Pages
104516 - 104516
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