Life–prediction for constant–stress fatigue in carbon–fibre composites

A detailed analysis has been carried out of the strength and fatigue behaviour under constant–stress cycling of four modern aerospace CFRP laminates, all having the common lay–up [(±45,02)2]s. Despite some important differences in their basic material characteristics, the fatigue responses of the four materials were similar. This pattern of behaviour has resulted in the development of a descriptive model of constant–life fatigue which has then been used as the basis for a life–prediction procedure. Preliminary attempts at validation of the method have met with a reasonable degree of success and suggest that it could provide designers with a means of selecting newly developed composites for fatigue applications on the basis of far less experimental data than are currently needed for confidence in design.

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