Delamination and debonding failure of laminated composite T-joints
Published: Jan 9, 2014
Abstract
Composites are increasingly being used in aerospace, automotive and other industries. The T-joint (also named stringer stiffened skin) is a typical connection, broadly used in thin-walled structures, such as the wing and fuselage of aircraft. This thesis presents the analysis of the delamination and debonding failure of laminated composite T-joints, in support of the design and manufacture of integrated composite structures. Major attention has...
Paper Details
Title
Delamination and debonding failure of laminated composite T-joints
Published Date
Jan 9, 2014
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