Fatigue failure of large fabricated structures can occur through the propagation of several small defects which either pre-exist in the structure as a result of the fabrication process or which initiate under the action of cyclic loading. The propagation of these small defects results in the coalescence of several small defects to form a dominant fatigue crack which then propagates to cause failure. In welded components such as the tubular joints of offshore jacket structures the dominant crack is often a semielliptical surface crack at the toe of the fillet weld. Existing methodologies offer simplistic approaches to predict the behaviour of adjacent surface defects. In general fracture mechanics offers a rational approach for the assessment of such problems.
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A Numerical and Experimental Study of the Development of Semi-Elliptical Fatigue Cracks by Defect Coalescence