For continuously welded structures subjected to cyclic loading, the highly stressed zones where cracks initiate and lead to failure are usually located at weld toes. At these critical points, called hotspots, the very local stress states are difficult to determine so that standard fatigue criteria are very diflicult to apply for fatigue life prediction. This work presents a fatigue design criterion for continuously welded thin sheet structures, based on a unique S-N curve. The approach, which refers to the hot-spot stress concept, defines the design stress S as the geometrical stress amplitude at the hot-spot.In practice, the geometrical stress state is calculated by means of the finite element method (FEM) using thin shell theory. Meshing rules for the welded connection, which can be applied methodically to any welding situation, allow the hot-spot location, and therefore the design stress of any structure, to be determined.Experimental data and FEM calculations show that a unique S-N curve can be obtained whatever the geometry of the welded structure and the loading mode. NOMENCLATURE e e = thickness of the attachment, and thickness of the plate. e!$fi$ = weld leg length on the attachment side, and on the plate side. I$), E p ) = shell element number i, perpendicular to the intersection curve of the shell element mean surfaces, on the attachment side, and on the plate side. Fi = load in the Oi direction. F,,, F-= maximum load and minimum load. @), n? = node number i, on the attachment side and on the plate side. N = number of cycles to fatigue failure. R = load ratio. = F,,,,,,/F,, S = design stress. uHs = geometrical stress at the hot spot. crL = actual stress at the hot spot (or local stress). AuHs = uHs range.