ICF13C

13th International Conference on Fracture June 16–21, 2013, Beijing, China -4- 0 45 90 135 -0.5 0.0 0.5 1.0 1.5 2.0 (c)  (Degree) a/c=0.2,r/a=0.008273,  =9.730 Klocal=0.200,Klocal/(2 r) 1/2=1.962 ij/Klocal/(2r)1/2 f33=Tz(f11+f22) f33=v(f11+f22) 11 f11 (T-stress neglected) 22 f22 33 f33=v(f11+f22) f11 f33=Tz(f11+f22) 0 45 90 13 0.0 0.5 1.0 1.5 2.0 (d) f33=v(f11+f22) f33=Tz(f11+f22)  (Degree) a/c=0.2, r/a=0.0075, =1.900 Klocal=0.1523, Klocal/(2r)1/2=3.5075 ij/Klocal/(2r)1/2 11(T-stress neglected) 22 33 f11 f22 f33=v(f11+f22) 11 f33=Tz(f11+f22) Fig.4 The angular distributions of stress components normalized by the local stress intensity factors in a normal plane of the quarter-elliptical corner crack front line. (a) through-the-thickness straight crack, (b) semi-elliptical surface crack, (c) quarter elliptical corner crack, (d) embedded elliptical crack. As shown in Fig. 4, the angular distributions of stress components in a normal plane of various crack front lines are given in the local Cartesian coordinates. It can be seen that 22 is in good agreement with f22, while the differences between 11 and f11 are great if the T-stress is neglected. When the T-stress is considered, the differences will become very small. In addition, the differences between 33 and f33 for the plane strain state (v(f11+ f22)) are great. If the Tz factor is considered in f33, f33 will be in good agreement with 33. 3. Three-parameter principle J–QT–Tz for the elastic-plastic material The HRR stress components can be expressed as           1 1 , , , , n ij m e ij m e Kr                (6) where   1 1 0 0 n J K I n             (7) σ0 is the yield stress. By considering the effects of geometry and size on crack-tip constraint, O’Dowd and Shih [8, 9] found that the near-tip stress field is governed by the two parameters of J and Q as follows:     1 1 0 0 0 0 n ij ij ij ij J r Q I n r J                            (8) The first term is the HRR solution ( 2    ), Q is a function of the stress triaxiality achieved ahead of the plane strain cracks. The λ is set to zero, then Qrr=Qθθ and Qij is the form

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