Fatigue crack growth testing of the Super CMV hollow shafts under combined torsional and axial loading

Fatigue crack growth tests were carried out on the hollow shaft specimens under combined torsional and axial loading. The effects of the shaft geometry, pre-cracks shapes and stress ratios, on the fatigue crack growth of hollow shaft specimens, were investigated. Experimental results show that up to four cracks around the holes, emanating from either pre-cracks, or the sites of the maximum tensile stress, were observed. Initially, the cracks were found to propagate under Mode I condition, on the maximum tensile stress plane, then veer towards the maximum shear stress plane, and propagate under a mixed Mode II and III condition. Fatigue crack growth rates, da dN , were characterised, using the semi-empirically determined power law relationship between da dN (in m/cycle) and ΔJ (in MPa m). The two constants for the correlation are 8.000 × 10−4 and 1.601, respectively.