Quantification of fibre bridging in Mode I cracked Glare without delaminations

Author:

Bhat Sunil,Narayanan S.

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference27 articles.

1. Fatigue crack growth modeling of fibre metal laminate (FML) composite;Abdullah;Eur. J. Sci. Res.,2009

2. Analytical prediction model for fatigue crack propagation and delamination growth in Glare;Alderliesten;Int. J. Fat,2007

3. On the available relevant approaches for fatigue crack propagation prediction in Glare;Alderliesten;Int. J. Fat,2007

4. Fatigue and damage tolerance issues of Glare in aircraft structures;Alderliesten;Int. J. Fat,2006

5. The meaning of threshold fatigue in fibre metal laminates;Alderliesten;Int. J. Fat,2009

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