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Off-axis Fatigue Crack Growth and the Associated Energy Release Rate in Composite Laminates
Authors:J Tong  F J Guild  S L Ogin  P A Smith
Affiliation:(1) Department of Materials Science and Engineering, University of Surrey, Guildford, Surrey, GU2 5XH, U.K
Abstract:Stable matrix crack growth behaviour under mechanical fatigue loading hasbeen studied in a quasi-isotropic (0/90/-45/+45)s GFRPlaminate. Detailed experimental observations were made on the accumulationof cracks and on the growth of individual cracks in +45° as well as 90° plies. A generalised plain strain finiteelement model of the damaged laminate has been constructed. This model hasbeen used to relate the energy release rate of growing cracks to the crackgrowth rate via a Paris relation.
Keywords:quasi-isotropic laminates  off-axis fatigue crack growth  energy release rate  finite element analysis
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