Fatigue results for both constant-amplitude and random loading are compared on basis of time to failure, where equivalent time to failure based on natural period of vibration is used for constant-amplitude tests; failure occurs sooner for random than for constant-amplitude loading at lower stress levels; at higher stress levels reverse condition is true; pertinence to aircraft structural components.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Experimental investigation of effects of random loading on fatigue life of notched cantilever-beam specimens of 7075-t6 aluminum alloy


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    Fralich, R.W. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :