Axisymmetric mode of deformation of cylinders subjected to compressive end loads is examined with aid of available theory; stresses and deformations obtained with theory are compared with those of 7075-T6 Al-alloy cylinder with high internal pressure; behavior of cylinder was in agreement with predictions; pertinence to aircraft fuselage and missiles.


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    Titel :

    Structural behavior of pressurized, ring-stiffened, thin-wall cylinders subjected to axial compression


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Peterson, J.P. (Autor:in) / Dow, M.B. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :