Test results discussed with reference to present knowledge of fatigue of materials and joints used in aircraft construction.


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    Title :

    Fatigue strength and related characteristics of aircraft joints -- II -- Fatigue characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and R303- T275 aluminum alloys


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Russell, H.W. (author) / Jackson, L.R. (author) / Grover, H.J. (author) / Beaver, W.W. (author)


    Publication date :

    1948


    Size :

    97 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English