The behavior of short and long fatigue cracks in the widely used damage tolerant aluminum alloy 2024-T3 was compared using flight simulation loading representatives for the Fokker 100 wing/fuselage structure. The results showed that the apparently anomalous behavior of short cracks is not significant for durability analysis of the current wing/fuselage structure. Also the data provide a reference for evaluating new, candidate materials for durable wing/fuselage structures in transport aircraft.


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    Titel :

    Short and Long Fatigue Crack Growth in 2024-T3 under Fokker 100 Spectrum Loading


    Beteiligte:
    R. J. H. Wanhill (Autor:in) / L. Schra (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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