IN the design of aircraft structures for fatigue strength, it is as well to bear in mind that those parts most likely to give trouble fatigue-wise are those wherein rivets or bolts have to react a load. The term ‘react’ is used here to distinguish this from the case where rivets or bolts arc used to hold the skin on the frame, etc., where the worst possible concentration of stress in terms of the nominal gross area will approach that of a hole in an infinitely wide sheet, or about 3·0. The riveted joint is more likely to approach that of a lug, which, for conventional rivet spacing and edge distance would be about 5½ in terms of gross stress. In other words, our working stress for a joint would be about one-half the axial stress in a plain sheet with holes for the same life. Other things, such as normal loads and buckling, may alter this ratio somewhat.


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    Titel :

    The Fatigue Strength of Riveted Joints


    Untertitel :

    An Experimental Study of the Factors Influencing the Life of Riveted Joints


    Beteiligte:
    Smith, C.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.1957


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Fatigue strength of riveted joints and lugs

    Schijve, J. | Engineering Index Backfile | 1956


    The Strength of Riveted Joints

    Bowen, I.G. | Emerald Group Publishing | 1945


    Frictional strength of riveted joints

    Weinblum, G. | Engineering Index Backfile | 1929


    Fatigue Crack Growth in Riveted Joints

    Fawaz, S. A. / Schijve, J. / De Koning, A. U. et al. | British Library Conference Proceedings | 1997


    Fatigue Crack Growth Predictions in Riveted Joints

    Fawaz, S. A. / Schijve, J. / United States; National Aeronautics and Space Administration et al. | British Library Conference Proceedings | 1999