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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    Title :

    Plastic buckling of eccentrically stiffened circular cylindrical shells


    Additional title:

    AIAA J


    Contributors:
    Jones, R.M. (author)

    Published in:

    AIAA Journal ; 5 , n 6


    Publication date :

    1967


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :