Effect of hexagonal stringer design on bulging factor and stress intensity factor of cracks in the skin of pressurized aircraft fuselage
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DOI: 10.1177/09544100221107724
Abstract: Aircraft structural fatigue is a serious issue. Untreated, it could lead to failure. Several aircraft accidents were caused by widespread fatigue damage. For cracks in the fuselage, the stress state is due to the bulging… read more here.
Keywords: stress intensity; bulging factor; fuselage; intensity factor ... See more keywords