A B S T R A C TThe aim of this work is to present an engineering method based on linear elastic finite element (FE) analyses oriented to fatigue strength assessments of fillet-welded joints made of steel or aluminium alloys and subjected to mode I loading in the weld toe region where fatigue cracks nucleate. The proposed approach combines the robustness of the notch stress intensity factor approach with the simplicity of the so-called 'peak stress method'. Fatigue strength assessments are performed on the basis of (i) a well-defined elastic peak stress evaluated by FE analyses at the crack initiation point (design stress) and (ii) a unified scatter band (design fatigue curve) dependent on the class of material, i.e. structural steel or aluminium alloys. The elastic peak stress is calculated by using rather coarse meshes with a fixed FE size. A simple rule to calculate the elastic peak stress is also provided if a FE size different from that used in the present work is adopted. The method can be applied to joints having complex geometry by adopting a two-step analysis procedure that involves standard finite element (FE) models like those usually adopted in an industrial context. The proposed approach is validated against a number of fatigue data published in the literature.Keywords coarse mesh; fatigue design; fillet-welded joints; finite element analysis; local approaches; notch stress intensity factors.
N O M E N C L A T U R Ea = crack length, V-notch depth or component's reference dimension a eff = effective component's dimension a 0 = El Haddad-Smith-Topper length parameter a N 0 = characteristic length that depends on a 0 and 2α d = adopted finite element size K I = mode I stress intensity factor K th = threshold range of the mode I stress intensity factor K V I , K V II = mode I, mode II notch stress intensity factor (NSIFs) of a sharp V-notch K V I , K V I I = range of K V I , K V II r, θ = polar coordinates T σ = scatter index defined as the ratio between the fatigue strengths for survival probability of 2.3 and 97.7% at a given number of cycles 2α = V-notch opening angle λ 1 , λ 2 = mode I and mode II eigenvalues in Williams' solution σ n , σ n = nominal stress, range of σ n σ peak , σ peak = linear elastic peak stress calculated by FEM at the sharp V-notch tip by means of a given mesh pattern, range of σ peak σ rr , σ θθ = stress components in a polar frame of reference σ th = fatigue strength at the knee point of a component in terms of nominal stress rangeCorrespondence: G. Meneghetti.