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Fatigue strength,crack initiation and propagation behavior of rolled AZ31B magnesium alloy plate were investigated. Axial tension-compression fatigue tests were carried out with cylindrical smooth specimens.Two types of specimens were machined with the loading axis parallel(L-specimen)and perpendicular(T-specimen)to rolling direction.Monotonic compressive 0.2%proof stress,tensile strength and tensile elongation were similar for both specimens.On the other hand,monotonic tensile 0.2%proof stress of the L-specimen was slightly higher than that of the T-specimen.Moreover,monotonic compressive 0.2%proof stresses were lower than tensile ones for both specimens.The fatigue strengths of 107cycles of the L-and T-specimens were 95 and 85 MPa,respectively. Compared with the monotonic compressive 0.2%proof stresses,the fatigue strengths were higher for both specimens.In other words, the fatigue crack did not initiate and propagate even though deformation twins were formed in compressive stress under the cyclic tension-compression loading.The fatigue crack initiated at early stage of the fatigue life in low cycle regime regardless of specimen direction.The crack growth rate of the L-specimen was slightly lower than of the T-specimen.Consequently,the fatigue lives of the L-specimen were longer than those of the T-specimen in low cycle regime.
Fatigue strength, crack initiation and propagation behavior of rolled AZ31B magnesium alloy plates were investigated. Two types of specimens were machined with the loading axis parallel (L-specimen) and perpendicular ( T-specimen) to rolling direction. Montonic compressive 0.2% proof stress, tensile strength and tensile elongation were similar for both specimens. On the other hand, monotonic tensile 0.2% proof stress of the L-specimen was slightly higher than that of the T -specimen. Moreover, monotonic compressive 0.2% proof stresses were lower than tensile ones for both specimens. fatigue strengths 107cycles of the L-and T-specimens were 95 and 85 MPa, respectively. Compared with the monotonic compressive 0.2% , the fatigue strengths were higher for both specimens.In other words, the fatigue crack did not propagate even though deformation twins were formed in compressive stress un der the cyclic tension-compression loading. fatigue fracture initiated early stage of the fatigue life in low cycle regime regardless of specimen direction. crack growth rate of the L-specimen was slightly lower than of the T-specimen. Conclusion, the fatigue lives of the L-specimen were longer than those of the T-specimen in low cycle regime.