Abstract
Location where delamination occurs in a balanced, symmetric laminate with free edge under uniaxial mechanical loading and/or hygrothermal expansion is predicted by comparing the energy release rates due to delamination growth from the free edge on various interfaces. The change of release rate with the delamination crack length is obtained by utilizing the conventional finite element method. And a new method is proposed to evaluate a saturated value of energy release rate in the delamination crack extension. The saturated value of energy release rate is used as a measure to predict the occurrence of delamination which has yielded good agreement with observations on tension—tension and compression—compression fatigue tests conducted on carbon—epoxy composite laminates.
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© 1987 Elsevier Applied Science Publishers Ltd
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Kondo, K., Aoki, T. (1987). An Energy Release Rate Approach for Free-edge Delamination Problem in Composite Laminates. In: Marshall, I.H. (eds) Composite Structures 4. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-3457-3_19
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DOI: https://doi.org/10.1007/978-94-009-3457-3_19
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-8048-4
Online ISBN: 978-94-009-3457-3
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