For reasons stated bolted connections on aircraft develop play and resultant backlash may impair safety of craft; author seeks to determine connection between stress range, load cycles and increase in play for normal eyebolt so that part can be replaced when it has reached statistical endurance limit. Brief English abstract from Luftfahrtforschung v 19 n 4 May 6 1942.


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    Titel :

    Development of play in bolted joints under fatigue


    Weitere Titelangaben:

    Aircraft Production


    Beteiligte:
    Dirksen, B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1942


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Nut Resilience and Vibration Fatigue Limit of Bolted Joints

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