Numerical and experimental investigation of fitting tolerance effects on damage and failure of CFRP/Ti double-lap single-bolt joints
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DOI: 10.1016/j.ast.2018.04.042
Abstract: Abstract CFRP/Ti bolted joints are increasingly used in aircraft structures. Optimizing the joint design is vital for overall composite structure designs. Therefore, a progressive damage model was developed for investigating the effects of clearance and… read more here.
Keywords: damage failure; cfrp double; double lap; failure cfrp ... See more keywords