Fatigue life of metal part subjected to spectrum of load intensities cannot be adequately evaluated from results of constant stress vs cycles (S-N curve) experiment alone; experiments were conducted for different materials and under different loading conditions; review of data reveals conflicting conclusions; approach is suggested which would take into consideration differences, and yield solution which coincides with each of individual results; spectral loading problem is worked out, demonstrating application of approach to reliability prediction.
Cumulative fatigue damage due to spectral loading
SAE -- Aerospace Reliability Maintainability Conference -- Proc
Proceedings of the 3rd SAE on Aerospace Reliability and Maintainability Conference, ; 1964 Fatigue
1964
4 pages
Aufsatz (Konferenz)
Englisch
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Cumulative Fatigue Damage due to Spectral Loading
SAE Technical Papers | 1964
|Cumulative Fatigue Damage Assessment
NTIS | 1964
Cumulative Fatigue Damage Assessment
NTIS | 1965
Cumulative Fatigue Damage Assessment
NTIS | 1964
Cumulative Fatigue Damage Assessment
NTIS | 1964