A B S T R A C T An experimental method was developed to quantify the multi-site fatigue crack initiation behaviour of engineering alloys in four-point bend fatigue testing under stress control. In this method, fatigue crack initiation sites [fatigue weak-links (FWLs)] were measured on the sample surface at different cyclic stress levels. The FWL density in an alloy could be best described using a three-parameter Weibull function of stress, although other types of sigmoidal functions might also be used to quantify the relation between weak-link density and stress. The strength distribution of the FWLs was derived from the Weibull function determined by fitting the weak-link versus stress curve experimentally obtained. As material properties, FWL density and strength distribution could be used to characterize the fatigue crack nucleation behaviour of engineering alloys quantitatively and evaluate the alloy quality in terms of weak-link density and strength distribution. In this work, the effects of environment, types of microstructural heterogeneities and loading direction on FWLs were all studied in detail in AA7075 T651, AA2026 T3511, A713 alloys, etc. It was also found that FWL should be quantified as a Weibull-type function of strain instead of stress, when the applied maximum cyclic stress exceeded the yield strength of the tested alloy.Keywords A713 cast Al alloy; four-point bend fatigue test; fatigue weak-link (FWL) density; high strength Al alloy; multi-site fatigue crack nucleation; strength distribution.
N O M E N C L A T U R EC = a scaling constant FIB = focused ion beam FEA = finite element analysis FWL = fatigue weak-link HCF = high-cycle fatigue k = constant L = rolling m = Weibull modulus n = the characteristic strength distribution of FWLs N = the number of fatigue weak-links at a specific stress level N 0 = the fatigue weak-link density OM = optical microscopy RH = relative humidity S = short transverse SEM = scanning electron microscopy T = long transverse ε = the strain associated with the applied stress σ ε 0 = the strain measured at stress of the fatigue limit σ 0 σ = stress level σ s = the ultimate tensile strength σ 0 = fatigue limit Correspondence: T. Zhai.