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Published in 2019 at "Engineering Failure Analysis"
DOI: 10.1016/j.engfailanal.2019.06.061
Abstract: Abstract This study focused on the numerical analysis of a cracked fuselage panel of an airplane on the basis of new nonlinear fracture mechanics parameters and concepts. Through finite element analysis (FEA) of the fragment…
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Keywords:
panel biaxial;
biaxial loading;
panel;
fuselage panel ... See more keywords