Simulating damage and delamination in fibre metal laminate joints using a three-dimensional damage model with cohesive elements and damage regularisation

Author:

Frizzell R.M.,McCarthy C.T.,McCarthy M.A.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference27 articles.

1. Towards application of fibre metal laminates in large aircraft;Vlot;Aircraft Eng Aerospace Technol,1999

2. GLARE technology development 1997–2000;Gunnink;Appl Compos Mater,2002

3. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J Mater Process Technol,2000

4. de Vries TJ. Blunt and sharp notch behaviour of glare laminates PhD. Delft University of Technology, Faculty of Aerospace Engineering; 2001.

5. Progressive damage modeling in fiber-reinforced materials;Lapczyk;Compos Part A,2007

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