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Fatigue life prediction of glass fibre-reinforced plastics using the acousto-ultrasonic technique

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Composite materials possess the characteristics of high stiffness and high fatigue strength which are desirable for advanced aircraft components. However, the fatigue behaviour of such materials depends upon a variety of factors (such as fibre volume fraction, percentage of voids and lay-up order), the effects of which are difficult to establish individually, so that a wholistic approach is the only satisfactory solution. The present paper deals with a nondestructive evaluation technique, which is a combination of acoustic emission and ultrasonics, for the evaluation of the fatigue life of a cross-plied ( 0° 90°) glass fibre-reinforced plastic composite. The results show that the fatigue life can be determined from the parameter known as the stress wave factor with the required degree of confidence. © 1987.

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