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Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer
Sayar, B., Kayran, A.Volume:
37
Language:
english
Journal:
Fatigue & Fracture of Engineering Materials & Structures
DOI:
10.1111/ffe.12127
Date:
May, 2014
File:
PDF, 2.34 MB
english, 2014