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.


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    Titel :

    Cumulative fatigue damage due to spectral loading


    Weitere Titelangaben:

    SAE -- Aerospace Reliability Maintainability Conference -- Proc


    Beteiligte:
    Harris, J.P. (Autor:in) / Lipson, C. (Autor:in)

    Kongress:

    Proceedings of the 3rd SAE on Aerospace Reliability and Maintainability Conference, ; 1964 Fatigue



    Erscheinungsdatum :

    1964


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :