FEM based fatigue crack growth predictions for spar of light aircraft under variable amplitude loading

Published 2012 View Full Article

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Title
FEM based fatigue crack growth predictions for spar of light aircraft under variable amplitude loading
Authors
Keywords
-
Journal
ENGINEERING FAILURE ANALYSIS
Volume 26, Issue -, Pages 50-64
Publisher
Elsevier BV
Online
2012-08-04
DOI
10.1016/j.engfailanal.2012.07.003

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