Issue 35

S. Morita et alii, Frattura ed Integrità Strutturale, 35 (2016) 82-87; DOI: 10.3221/IGF-ESIS.35.10 85 R ESULTS AND DISCUSSION he relationship between the crack growth rate ( da/dN ) and the  K is shown in Fig.4. The figure shows that the da/dN of the L-S specimen was several times lower than that of the L-T and S-T specimens in the examined  K . The da/dN of the S-T specimen was higher than that of the L-T and L-S specimens in the examined  K . Fig. 5 shows the typical SEM images of the fatigue tested L-T, L-S, and S-T specimens. Many straight lines or steps were observed over several grains along with the macroscopic direction of fatigue crack growth in the L-T specimen (Fig.5(a) and (b)). In contrast, in the L-S specimen, many lines or steps perpendicular to the macroscopic direction of fatigue crack growth were observed (Fig.5(c) and (d)). The fracture surface of the L-T and L-S specimens had a similar morphology and did not depend on  K . On the other hand, various quasi-cleavage facets independent of the macroscopic direction of fatigue crack growth were observed in the S-T specimen (Figs.5(e) and (f)). Moreover, the fracture surface roughness at low  K , up to  K = 7 MPa·m 1/2 , was larger than that at high  K , above  K > 7 MPa·m 1/2 . The macroscopic fatigue crack propagation is parallel to the a -axis (perpendicular to basal plane) of each grain for the L-T specimen, and parallel to the c -axis (perpendicular to basal plane) of each grain for the L-S specimen. Therefore, it is inferred that the c -axis direction is unfavorable for the fatigue crack propagation in rolled AZ31B magnesium alloy. It is also found that the macroscopic fatigue crack propagation is various directions to the a -axis (parallel to basal plane) of each grain in the S-T specimen. Thus, it appears that the fatigue crack propagated easily in a direction parallel to the a -axis (parallel to basal plane) of each grain in the S-T specimen. In addition, the deformation twinning of polycrystalline magnesium alloys plays an important role in the deformation process because of the limitation of slip system. When the specimens were subjected to a stress higher than the compressive and tensile yield stress in the load-controlled fatigue test, deformation twins were observed in the extruded magnesium alloys [3, 4, 26]. In contrast, free deformation twins are observed around the fatigue crack path (within the plastic zone) in the L-T and L-S specimens. It appears that the fatigue crack growth is not controlled by the deformation twinning at a crack tip in textured polycrystalline magnesium alloys. Figure 4 : Relationship between crack growth rate and stress intensity factor range. C ONCLUSIONS he fatigue crack propagation behaviors of three types of specimens of textured polycrystalline magnesium alloy, in which the macroscopic fatigue crack propagated perpendicular to and parallel to the basal plane of each grain, has been investigated. It is found that the a -axis direction is favorable for the fatigue crack propagation in textured T T