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Fatigue life estimation of graphite/epoxy laminates under consideration of delamination growth

โœ Scribed by H. W. Bergmann; R. Prinz


Publisher
John Wiley and Sons
Year
1989
Tongue
English
Weight
931 KB
Volume
27
Category
Article
ISSN
0029-5981

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โœฆ Synopsis


A closed form approach to the assessment of the fatigue life of graphite'epoxy laminates under cyclic tension xornpression loading has been developed. The model is mechanistic and uses cyclic energy release rates for prediction of delamination growth and of critical delamination sizes which induce buckling and the final failure of the laminates. Tests performed with graphitr,'epoxy specimens of stacking order [On, $ m ] s with scvered central plies "$3, and of stacking order [0,.+45, 0,.-45, 0. 901% with a central unloaded hole.

indicate good correlation betwcen estimated values and observed delamination growth, critical buckling strength of separated plies and load cycles to failure.


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microscopes, ekctrrmic flash light sources, cl~~y operated 35mm cameras and pro~mrn~ components to allow exposures to be mfdc at lnaximum tension load at predetarmined cyclic times without interrupting the fatigue test. Prior to testing, the notch roots of the specimens were polished in a polishing