Basic assumptions of conventional riveted joint design practice are discussed with respect to their applicability to aluminum alloys; data presented to establish effect of holes on tension efficiency of 24ST aluminum alloy sheet, and values are proposed for use in riveted joint design. Before Inst Aeronautical Sciences.


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    Title :

    Tension joints in aircraft structures


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1943


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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