Experiments are described in which notched specimens of 2024-T351 aluminum alloy were subjected to fatigue load distribution typical of that encountered by aircraft operating continuously at low altitude; they serve to demonstrate effects of design stress level on life and suggest that lives of general-purpose aircraft currently used in these roles may be as low as 2000 to 3000 hrs; other findings. (48492)


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    Title :

    Fatigue tests on notched specimens of 2024-T351 aluminum alloy under low altitude aircraft load spectrum


    Additional title:

    Nat Res Counc Can, Aeronaut Rep


    Contributors:


    Publication date :

    1968


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English