PSI - Issue 24

Giovanni Meneghetti et al. / Procedia Structural Integrity 24 (2019) 190–203 Meneghetti et al./ Structural Integrity Procedia 00 (2019) 000–000

200

11

(b)

(a)

S355J2

S355J2

crack at toe

ADI 1050

ADI 1050

ADI 1050

S355J2

S355J2

Specimen code: C11_1, AW, 4PB loading, R= 0.05, Δσ = 322 MPa, N f = 782127 cycles

Fig. 9. Fracture surfaces of cruciform nlc fillet-welded joints tested under four-point-bending fatigue loading. Finally, Figs. 10-13 show that all tested welded details exhibit an endurable stress range, which is referred to a survival probability of 97.7% and 2 million loading cycles, higher than the FAT values suggested by Eurocode 3 and IIW Recommendations (Eurocode 3 (2005); Hobbacher (2016)) for corresponding homogeneous joints made of structural steels, especially at the medium-high cycle fatigue regime.

2000

Δσ A,97.7% = 73 MPa N A = 2 ∙10 6 cycles Scatter Index (2.3%-97.7%): T σ = 139/73 = 1.91 Slope k = 4.88

nominal stresses calculated in the weld throat area from Eq. (1)

Scatter band calibrated on experimental results

1000

139 100 73

100

36 (k =3)

Dissimilar ADI 1050-S355J2 welded joints Steel welded joints - fatigue curve from IIW and Eurocode 3

Nominal stress range Δσ [MPa]

Partial-penetration butt-joints, R = 0.05

N A

10

1.E+04

1.E+05

1.E+06

1.E+07

Number of cycles to failure, Nf

Fig. 10. Experimental results of axial fatigue tests performed on partial-penetration butt-joints; nominal axial stress range evaluated in the weld throat area.