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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fatigue life estimates for helicopter loading spectra


    Contributors:


    Publication date :

    1990-07-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Fatigue life estimates for helicopter loading spectra

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


    Fatigue life estimates for helicopter loading spectra

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


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Trans Tech Publications | 2014


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Tema Archive | 2014