Precipitate-mediated fatigue crack propagation behavior of Al-Zn-Mg-Cu alloy tailored by non-isothermal aging

The fatigue crack propagation behavior of non-isothermally aged Al-Zn-Mg-Cu alloy was examined at different aging stages. It has been revealed that non-isothermal aging (NIA) improved the fatigue crack resistance by adjusting the thermodynamics, and thus modified the precipitation configuration. Enhanced crack propagation threshold and decreased crack propagation rate were achieved when NIA was applied and carried out thoroughly. Fine and dispersed GP zones existing in underaged alloy significantly intensified the slip localization, which effectively mitigated the stress concentration near the crack tip and showed an approximately 8.2 MPa & sdot;m1/2 & sdot; m 1/2 crack propagation threshold. Smaller width of the precipitate-free zone enabled the slip bands to propagate through the grain boundaries. However, relatively low strength and intense slip localization led the fatigue crack to propagate along the crystallographic slip bands, responsible for the higher crack propagation rate. For minorly over-aged alloys, coarsening and elevated number density of intragranular precipitate effectively hindered the movement of dislocation around, where strain concentration was frequently and preferentially induced, causing the degradation of resistance to fatigue crack propagation.