The strain energy release rate of delamination in fabric-reinforced composites

G. Marom; I. Roman; H. Harel; M. Rosensaft; S. Kenig; A. Moshonov

doi:10.1016/0143-7496(88)90028-0

The strain energy release rate of delamination in fabric-reinforced composites

G. Marom^*
, I. Roman
, H. Harel
, M. Rosensaft
, S. Kenig
, A. Moshonov

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

12 Scopus citations

Abstract

Mode I and Mode II delamination fractures are investigated in glass, carbon and Kevlar fabric-reinforced composites. The effects of the angle of reinforcement and of the fibre volume content are examined particularly. The main conclusion is that in designing a fabric-reinforced composite for maximum resistance to delamination, the axes of the fabric must form an angle of 45° with respect to the expected delamination direction.

Original language	English
Pages (from-to)	85-91
Number of pages	7
Journal	International Journal of Adhesion and Adhesives
Volume	8
Issue number	2
DOIs	https://doi.org/10.1016/0143-7496(88)90028-0
State	Published - Apr 1988

Keywords

angle of reinforcement
delamination fractures
design
fabric-reinforced composites
failure modes
fibre volume content
strain energy release rates

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10.1016/0143-7496(88)90028-0

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title = "The strain energy release rate of delamination in fabric-reinforced composites",

abstract = "Mode I and Mode II delamination fractures are investigated in glass, carbon and Kevlar fabric-reinforced composites. The effects of the angle of reinforcement and of the fibre volume content are examined particularly. The main conclusion is that in designing a fabric-reinforced composite for maximum resistance to delamination, the axes of the fabric must form an angle of 45° with respect to the expected delamination direction.",

keywords = "angle of reinforcement, delamination fractures, design, fabric-reinforced composites, failure modes, fibre volume content, strain energy release rates",

author = "G. Marom and I. Roman and H. Harel and M. Rosensaft and S. Kenig and A. Moshonov",

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AU - Marom, G.

AU - Roman, I.

AU - Harel, H.

AU - Rosensaft, M.

AU - Kenig, S.

AU - Moshonov, A.

PY - 1988/4

Y1 - 1988/4

N2 - Mode I and Mode II delamination fractures are investigated in glass, carbon and Kevlar fabric-reinforced composites. The effects of the angle of reinforcement and of the fibre volume content are examined particularly. The main conclusion is that in designing a fabric-reinforced composite for maximum resistance to delamination, the axes of the fabric must form an angle of 45° with respect to the expected delamination direction.

AB - Mode I and Mode II delamination fractures are investigated in glass, carbon and Kevlar fabric-reinforced composites. The effects of the angle of reinforcement and of the fibre volume content are examined particularly. The main conclusion is that in designing a fabric-reinforced composite for maximum resistance to delamination, the axes of the fabric must form an angle of 45° with respect to the expected delamination direction.

KW - angle of reinforcement

KW - delamination fractures

KW - design

KW - fabric-reinforced composites

KW - failure modes

KW - fibre volume content

KW - strain energy release rates

UR - https://www.scopus.com/pages/publications/0023994315

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JO - International Journal of Adhesion and Adhesives

JF - International Journal of Adhesion and Adhesives

IS - 2

ER -

The strain energy release rate of delamination in fabric-reinforced composites

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Keywords

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