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Predicting delamination and debonding in modern aerospace composite structures

✍ Scribed by G.A.O. Davies; D. Hitchings; J. Ankersen


Book ID
108103975
Publisher
Elsevier Science
Year
2006
Tongue
English
Weight
412 KB
Volume
66
Category
Article
ISSN
0266-3538

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Experimental studies on the failure mode of composite T-joint specimens, in the presence of adhesive interlaminar layers, are presented. Tests underline the role played by the interaction between delamination and debonding phenomena. Quasi static analyses of the tests are performed by means of expli