Paper shows how to obtain ordinary differential equations which determine distributed stresses when concentrated load is applied to ring of reinforced thin-walled cylinder; general approach developed permits applied force to have arbitrary direction; account is taken of flexure perpendicular to plane and torsion and flexure in plane; strain energy is taken to consist of 5 separate terms which are given; pertinence to aircraft fuselages and rockets.


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    Title :

    Theory of ring-stiffened cylinders


    Additional title:

    J Aerospace Sciences


    Contributors:

    Published in:

    Journal of Aerospace Science ; 28 , n 9 ; p 702-709


    Publication date :

    1961


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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