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A Multiaxial Variable Amplitude Fatigue Life Prediction Method Based on a Plane Per Plane Damage Assessment

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Figure

Figure 1. Flow chart of the plane per plane fatigue life assessment method.
Figure 3. Problem of cycle’s identification for a multiaxial variable amplitude stress states histoty
Figure 6. Identification of a multiaxial stress states cycle.
Figure 8. Distribution of the fatigue indicator Eh : (a) for a constant principal stress directions cycle, b) for a rotating principal stress directions cycle
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