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Finite Element Interface Technology for Modeling Delamination Growth in Composite Structures

✍ Scribed by Pantano, Antonio; Averill, Ronald

Book ID
126522923
Publisher
American Institute of Aeronautics and Astronautics
Year
2004
Tongue
English
Weight
576 KB
Volume
42
Category
Article
ISSN
0001-1452

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## Abstract The finite element analysis of delamination in laminated composites is addressed using interface elements and an interface damage law. The principles of linear elastic fracture mechanics are indirectly used by equating, in the case of single‐mode delamination, the area underneath the tr