Computational assessment of nonlinear fracture resistance parameters for cracked fuselage panel under biaxial loading
Sign Up to like & getrecommendations! 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… read more here.
Keywords: panel biaxial; biaxial loading; panel; fuselage panel ... See more keywords