Investigation of the load sequence effects in fatigue of damaged composite laminate & characterization of fatigue damage-Reference-Cited by-同舟云学术

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Investigation of the load sequence effects in fatigue of damaged composite laminate & characterization of fatigue damage

Published:2010-04 Issue:2-3 Volume:63 Page:565-569
ISSN:0972-2815
Container-title:Transactions of the Indian Institute of Metals
language:en
Short-container-title:Trans Indian Inst Met

Author:

Duragkar M. S.,Paretkar R. K.,Peshwe D. R.,Paranjpe S. A.

Publisher

Springer Science and Business Media LLC

Link

http://link.springer.com/content/pdf/10.1007/s12666-010-0083-0.pdf

Reference13 articles.

1. Hahn H T and Kim R Y, Fatigue behaviour of composite laminates, J. Composite Mat., 10 (1976) 156.

2. Johnson W S, Mechanisms of fatigue damage in boron/aluminum composite, ASTM STP 775, Philadelphia, PA, (1982) 83.

3. Johnson, WS., Modeling stiffness loss in boron/aluminum laminates below the fatigue limit, ASTM STP 813, Philadelphia, PA, (1983) 160.

4. O’Brien, TK., Characterization of delamination onset and growth in a composite laminate, ASTM STP 775, Philadelphia, PA, (1982) 140.

5. Daniel, I M and Charewicz A, Fatigue damage mechanisms and residual properties of graphite/epoxy laminates, Engg. Fract. Mech., 25 (1986) 793.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Review and Assessment of Fatigue Delamination Damage of Laminated Composite Structures;Materials;2023-12-16

2. Effect of Post-Cathodic EPD Acetone Washing of Carbon Fibres on the Mechanical Properties of Graphene Carboxyl Embedded CFRP Composites;Transactions of the Indian Institute of Metals;2022-03-14

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