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

Published 2020 View Full Article

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Title
XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug
Authors
Keywords
XFEM, Fatigue crack growth, Wing-fuselage attachment lug, Light aerobatic aircraft
Journal
ENGINEERING FAILURE ANALYSIS
Volume 112, Issue -, Pages 104516
Publisher
Elsevier BV
Online
2020-03-28
DOI
10.1016/j.engfailanal.2020.104516

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