Application of the Hartman–Schijve equation to represent Mode I and Mode II fatigue delamination growth in composites

Author:

Jones R.,Pitt S.,Bunner A.J.,Hui D.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference57 articles.

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3. Raizenne D. Case history: CF116 upper wing skin fatigue enhancement boron doubler, chapter. In: Baker A, Rose LRF, Jones R, editor. Advances in the Bonded composite repair of metallic aircraft structure. Elsevier Applied Science Publishers; 2002. ISBN 0-08-042699-9.

4. An experimental investigation into the effect of impact damage on the compressive strength of step lap joints;van Blaricum;Eng Fract Mech,1989

5. Wanhill RJH. Characteristic stress intensity factor correlations of fatigue crack growth in high strength alloys: reviews and completion of NLR investigations 1985-1990, NLR-TP-2009-256; September 2009.

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