Numerical and experimental investigation of fitting tolerance effects on damage and failure of CFRP/Ti double-lap single-bolt joints

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 interference sizes on the damage and failure of CFRP/Ti...

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Bibliographic Details
Published inAerospace science and technology Vol. 78; pp. 461 - 470
Main Authors Cao, Yuejie, Cao, Zengqiang, Zuo, Yangjie, Huo, Lubin, Qiu, Jianping, Zuo, Duquan
Format Journal Article
LanguageEnglish
Published Elsevier Masson SAS 01.07.2018
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