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Book chapter

Delamination fractures in composite materials

In Modelling Damage, Fatigue and Failure of Composite Materials — 2015, pp. 213-240
From

Department of Wind Energy, Technical University of Denmark1

Composites Mechanics and Materials Mechanics, Department of Wind Energy, Technical University of Denmark2

Delamination, that is, crack growth between different plies, is a common failure mode in laminated composites. Analysis, testing, and designing against delamination crack growth is discussed in the present chapter. In comparison with crack growth in isotropic metals, delamination is complicated by elastic orthotropy, mixed-mode crack growth, and large-scale bridging (LSB).

This draws attention to the need for dedicated fracture mechanics to test both specimens and theory in order to characterize delamination in a proper manner. For instance, J-integral specimens are preferred for the determination of bridging laws (traction-separation laws) to describe LSB. Micromechanical models describing toughening due to crack bridging are also briefly reviewed..

Language: English
Publisher: Woodhead Publishing
Year: 2015
Pages: 213-240
Series: Woodhead Publishing Series in Composites Science and Engineering
ISBN: 1782422862 , 1782422986 , 9781782422860 and 9781782422983
Types: Book chapter
DOI: 10.1016/B978-1-78242-286-0.00011-X
ORCIDs: Sørensen, Bent F.

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