Investigation being conducted on compressive strength of flat 24S-T aluminum alloy panels for aircraft; tests showed that effect of riveting on strength of panels depended on type of failure.


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    Title :

    Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners -- Panels of various lengths with close stiffener spacing


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Dow, N.F. (author) / Hickman, W.A. (author)


    Publication date :

    1947


    Size :

    18 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :