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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    Titel :

    Tension joints in aircraft structures


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Holleman, C.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1943


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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