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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Published in | Aerospace science and technology Vol. 78; pp. 461 - 470 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Masson SAS
01.07.2018
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Subjects | |
Online Access | Get full text |
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