Identification and modeling of fatigue crack growth mechanisms in a die-cast AM50 magnesium alloy

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We experimentally identified the fatigue crack growth micromechanisms operating near the limit plasticity regime in a commercial high-pressure die-cast AM50 alloy with a critical review of the available literature. An existing multistage fatigue model was modified to subsequently recognize these micromechanisms in a threefold fatigue crack growth regime. The formation of the main fatigue crack occurred almost exclusively at shrinkage pores and to a lesser extent at large Mn-rich particles. At shrinkage pores, several adjacent cracks typically incubated at the edge of flat interdendritic pores, propagated along the a-Mg dendrite cells/Al-rich eutectic interface, and rapidly coalesced into a main physically small fatigue crack that advanced through the Al-rich eutectic. In the long crack regime, the crack advanced in a mixed transdendritic–interdendritic mode along persistent slip bands spreading over several tens of dendrite cells. The model predicts well the fatigue life compared to the experimental data when these observed mechanisms are accounted for.


Fig. 1. Backscatter FEG-SEM micrographs of a polished AM50 sample cut from the grip section of a fractured fatigue specimen showing (a) an overall view of the microstructure depicting shrinkage pore clusters and an Al-rich eutectic layer fully occupying the dendrite cell boundaries, (b) a higher magnification image revealing the formation of the beta phase and Mn-rich phase inside the Al-rich eutectic layer.

The high strength-to-weight ratio of contemporary magnesium alloys that are suitable for ultimate weight reduction purposes in automotive and aircraft components has stimulated in the last decade substantial interest in understanding their fatigue crack growth behavior with process rationalization. Experimental observations on cast Mg alloys have accumulatively revealed that the dendrite cell size, pores, secondary phase particles, persistent slip bands and twinning in the dendrite cells considerably affect the fatigue durability and crack growth mechanisms of dendritic magnesium alloys [3–7].

Our interest of studying the AM50 alloy was motivated by the universal trend to reduce the aluminum content of Mg–Al alloys in an effort to increase ductility under impact and fatigue loading for automotive components. In this paper, relevant micromechanisms of fatigue crack growth in an AM50 alloy are carefully examined. Fatigue tests were carried out in a fully reversed strain control condition at strain amplitudes ranging from 0.1% to 0.7%. The microstructure before and after fatigue failure was analyzed by means of field emission gun-scanning electron microscopy (FEG-SEM) and electron probe microanalysis (EPMA) using specimens extracted from the grip regions and gage lengths of tested samples, respectively.

Fig. 2. Backscatter FEG-SEM micrographs of a polished AM50 sample cut from the grip section of a fractured specimen showing (a) the Al-rich eutectic layer surrounding continuously the dendrite cells and the b-phase is formed spreading in the center of the Al-rich eutectic layer, (b) a higher magnification image of an Mn-rich inclusion juxtaposed of two particles; the two overlying particles are substantially richer in Mn than the underlying darker particle corresponding to the Al8Mn5 phase, and (c) a secondary electron (SE) image of the same inclusion shown in (b), the underlying phase presents as an agglomeration of extremely small particles (5 nm in diameter).



Citation: Identification and modeling of fatigue crack growth mechanisms in a die-cast AM50 magnesium alloy, El Kadiri, H., Xue, Y., Horstemeyer, M.F., Jordon, J.B., Wang, P.T., Acta Materialia, v 54, n 19, p 5061-5076, November, 2006.

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