Research on the applicability of the Paris theory to aircraft riveted stiffened structures is reported. This research was carried out in two stages: evaluation of the stress intensity factor K in stiffened panels and measurement of crack growth rate in stiffened and unstiffened panels.


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    Title :

    Theoretical and Experimental Research on the Fatigue Crack Propagation in Stiffened Panels. An Evaluation of the Paris Theory


    Contributors:
    A. Salvetti (author) / A. Frediani (author) / E. Grassi (author) / F. Rossi (author)

    Publication date :

    1974


    Size :

    83 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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