Research Article
A Nonlinear Fatigue Damage Model Based on Equivalent Transformation of Stress
Table 9
Applied cycles and failure cycles under different stress amplitudes.
| Level | 1 | 2 | 3 | 4 |
| Stress amplitude/MPa | 260 | 275 | 290 | 305 | Applied cycle, n/cycle | 210,000 | 110,500 | 60,000 | 33,750 | Failure cycle, N/cycle | 840,000 | 442,000 | 240,000 | 135,000 |
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