Solution is derived by use of J2 deformation theory of plasticity for set of simply supported edge boundary conditions; uniaxial character of stiffeners and stiffener eccentricity (asymmetry about cylinder middle surface) are explicitly accounted for as is variable Poisson's ratio in plastic region; closed-form stability criterion is obtained for axial compression, lateral pressure, and hydrostatic pressure loadings; numerical example illustrates effect of plastic action on buckling load of typical aerospace structure.


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    Titel :

    Plastic buckling of eccentrically stiffened circular cylindrical shells


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Jones, R.M. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 6


    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :