Experiments are described in which notched specimens of 2024-T351 aluminum alloy were subjected to a fatigue load distribution typical of that encountered by an aircraft operating continuously at low altitude. While the experiments lack statistical validity, they serve to demonstrate the effects of design stress level on life and suggest that the lives of general-purpose aircraft currently used in these roles may be as low as 2000 to 3000 hours. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fatigue Tests on Notched Speciments of 2024-T351 Aluminum Alloy under a Low Altitude Aircraft Load Spectrum


    Beteiligte:
    J. A. Dunsby (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading

    DuQuesnay, D. L. / Yu, M. T. | British Library Online Contents | 1998



    Fatigue Behaviors of 2024 Aluminum Alloy under Aviation Load Spectrum

    CHEN Yajun / WANG Ailun / WANG Fusheng et al. | DOAJ | 2016

    Freier Zugriff