Several linear elastic fracture mechanics (LEFM) models have been deve
loped to simulate the fatigue performance of welded joints, particular
ly for offshore structures. Such models are used to estimate residual
life when cracks are discovered in service. These models are also used
to interpret available experimental results and may eventually be use
d in design. A key element to the success of such models is the realis
tic modelling of fatigue crack shape development. In all fatigue testi
ng of welded T-plate, pipe-plate and tubular joints in the Canadian Of
fshore Research Programme, care was taken to monitor crack shape devel
opment using beach marks and potential-drop techniques. Crack shape de
velopment was significantly influenced by specimen thickness, stress d
istribution and environment. A fatigue model is proposed which explici
tly models the growth and coalescence of multiple semi-elliptic fatigu
e cracks. Such a model has the potential of modelling geometry and env
ironmental effects through their influence on crack shape development.
The basics of this model, including coalescence and the calculation o
f stress intensity factors, are discussed. Verification studies involv
ing both T-plate and pipe-plate specimen geometries are presented.