Issue 36

M. Arsic et alii, Frattura ed Integrità Strutturale, 36 (2016) 27-35; DOI: 10.3221/IGF-ESIS.36.03 34 When substitute value fatigue strength of K-grooved butt welds, S = 420 MPa (Fig. 2), in Eq. 8 critical length of short crack will be a c =0.1 mm. On the basis of experimental examinations, values of fatigue notch factors k f for different initial fatigue cracks calculated by Eq. 2, are given in Tab. 5. Specimen class Initial fatigue crack, a [mm] Fatigue notch factor, k f 1 0.250 1.33 2 0.351 1.49 3 0.591 1.76 4 0.723 1.86 5 1.125 2.15 Table 5 : Values of fatigue notch factors. Results of fatigue crack growth testing Fatigue crack growth testing has been performed by the controlled bending force in three points, with asymmetrical load R= F min /F max = 0.5, on the specimen with edge notch. Testing has been carried out using high frequency pulsator "Cracktronic", and gathering of crack growth data has been done by using measuring foils ARM A-10. Number of cycles for the every 0.1 mm growth of crack has been recorded during experiment. Crack growth has been observed by magnifying glass (24 x). On the basis of these records, diagram a - N, Fig 10, has been drawn. Curve a - N indicates that fatigue crack grows slowly till a = 1.5 mm, when rapid crack growth occurs for relatively small number of load cycles. Relationship a - N can be taken as uniform, because there is no crack growth deceleration or its abrupt growth. Relationship a - N has been used as the basis for determination of crack growth rate, da/dN. In this paper, crack growth rates have been calculated by using the polynomial method, as defined in ASTM E647. Adequate range of stress intensity factor  K, depending on specimen shape, crack length and range of variable force  F = F max – F min , has been calculated. Values of coefficients m and C have been calculated, as they characterize resistance of material to crack growth and define Paris’ equation (m=3.516, C=3.18 ∙ 10 -12 ). Obtained values for m and C correspond to material class with similar mechanical properties, /3-5/. Relationship da/dN -  K is shown in Fig. 11. On the basis of numerous examinations, which showed that fatigue threshold has appeared for low values of crack growth rate, i.e. in rate range from 10 -6 up to 10 -8 mm/cycle, and according to the shape of da/dN -  K curve (Fig. 11), one can conclude that value of fatigue threshold is  K th = 7.24 MPa, corresponding to crack growth rate of 10 -8 mm/cycle. Figure 10 : Experimentally obtained a-N curve.