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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of play in bolted joints under fatigue


    Additional title:

    Aircraft Production


    Contributors:
    Dirksen, B. (author)

    Published in:

    Aircraft Production ; 4 , n 47 ; p 578


    Publication date :

    1942


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Spectrum fatigue of composite bolted joints

    Schon, J. / Nyman, T. | Tema Archive | 2002




    Numerical method for fatigue life of plane bolted joints under thermal load

    You, Ziyun / Fang, Yu / Liu, Xintian et al. | SAGE Publications | 2020