“…In fact, there are significant differences in the fatigue damage mechanisms of composites at different stress ratios, and the
plane is usually divided into compression‐compression (C‐C), compression‐tension (C‐T) and tension‐tension (T‐T) loading zones according to the value of the stress ratio
13,21 . However, a large number of comparative results of CLD models and fatigue test data indicate that the
plane should be divided into four zones that is, C‐C, C‐T, tension‐compression (T‐C) and tension‐tension (T‐T) loading zones,
31,32 as shown in Figure 5. Each load zone should be determined separately in the p ‐CLD modeling and the equal probability quantile points within each load zone should be co‐linear.…”