Prediction of Fatigue Crack Growth Rate and Stress Intensity Factors Using the Finite Element Method

Figure 10

For CT02 specimen, (a) FRANC2D/L, maximum principal stress, (b) ANSYS, maximum principal stress, (c) FRANC2D/L, minimum principal stress, and (d) ANSYS, minimum principal stress.

(a)

(b)

(c)

(d)