Helicopter loading histories applied to notch metal samples are used as examples, and their fatigue lives are calculated by using a simplified version of the local strain approach. This simplified method has the advantage that it requires knowing the loading history in only the reduced form of ranges and means and number of cycles from the rain-flow cycle counting method. The calculated lives compare favorably with test data.


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    Titel :

    Fatigue life estimates for helicopter loading spectra


    Beteiligte:
    Khosrovaneh, A. K. (Autor:in) / Dowling, N. E. (Autor:in) / Berens, A. P. (Autor:in) / Gallagher, J. P. (Autor:in)


    Erscheinungsdatum :

    01.07.1990



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Fatigue life estimates for helicopter loading spectra

    Khosrovaneh, A. K. / Dowling, N. E. / Berens, A. P. et al. | NTRS | 1989


    Fatigue life estimates for helicopter loading spectra

    Khosrovaneh, A.K. / Dowling, N.E. / Berens, A.P. et al. | Tema Archiv | 1990


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Trans Tech Publications | 2014


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Tema Archiv | 2014