Effect of stress ratio or mean stress on fatigue delamination growth in composites: Critical review

Author:

Khan Rafiullah,Alderliesten Rene,Badshah Saeed,Benedictus Rinze

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference103 articles.

1. George L. Roderick, Richard A. Everett, Jr, John H. Crews, Jr, Cyclic Debonding of unidirectional composite bonded to aluminum sheet for constant amplitude loading. NASA Technical Note TN D-8126; 1976.

2. Bathias C, Laksimi A. Delamination threshold and loading effect in fiber glass epoxy composite. Delamination and debonding of materials, ASTM STP Philadelphia; 1985. p. 10.

3. Ramkumar RL, Whitcomb JD. Charachterization of mode I and mixed mode delamination growth in T300/5208 graphite/epoxy. In: Delamination and debonding of materials. ASTM STP, vol. 876; 1985. p. 20.

4. Delamination fatigue crack-growth in unidirectional graphite epoxy laminates;Gustafson;J Reinf Plast Compos,1987

5. Effect of stress ratio on near-threshold propagation of delamination fatigue cracks in unidirectional CFRP;Hojo;Compos Sci Technol,1987

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