Delamination tolerance studies in laminated composite panels

Author:

Singh K L,Dattaguru B,Ramamurthy T S,Mangalgiri P D

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Reference13 articles.

1. Badari Narayana K, Dattaguru B, Ramamurthy T S, Vijayakumar K 1994 A general procedure for modified crack closure integral in 3D problems with cracks.Eng. Fracture Mech. 48: 167–176

2. Buchholz F G 1984 Improved formulae for the FE calculation of the strain energy release rate by the modified crack closure integral method.Proc., 4th World Congress and Exhibition in Finite Element Methods, Interlaken, pp 650–659

3. Broek D 1978Elementary engeneering fracture mechanics 2nd edn (Amsterdam: Sijthoff and Noordhoff) pp 74–82

4. De Georges D G, Maison S, Tallero D, Petitniot J L 1992 Buckling and post-buckling behavior of a delamination in a carbon-epoxy laminated structure: Experiments and modeling, debonding/delamination of composites. AGARD-CP-530, 7.1–7.11

5. Jones R, Callinan R, Teh K K, Brown K C 1984 Analysis of multi-layer laminates using three-dimensional super-elements.Int. J. Numer. Methods Eng. 20: 583–587

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