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    Nonlinear deformation and stability of supported oval cylindrical shells under torsion and bending with internal pressure

    Nonlinear deformation and stability of supported oval cylindrical shells under torsion and bending with internal pressure


    Abstract A problem of geometrically nonlinear deformation and stability of supported cylindrical shells with the oval cross-section contour is solved by the finite element method. The nonlinear deformation and stability of shells under combined loading by bending, torsion moments, transverse force and internal pressure are analyzed. The critical loads and buckling modes of shells are determined. The influence of deformation nonlinearity and shell ovality on critical loads is clarified.

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    Titel :

    Nonlinear deformation and stability of supported oval cylindrical shells under torsion and bending with internal pressure

    Beteiligte:
    Zheleznov, L. P. (Autor:in) / Kabanov, V. V. (Autor:in) / Boiko, D. V. (Autor:in)
    Erschienen in:

    Russian Aeronautics (Iz VUZ) ; 53 , 4 ; 466-469

    Erscheinungsdatum :

    2010-12-01

    Format / Umfang :

    4 pages

    ISSN :

    1934-7901 , 1068-7998

    DOI :

    https://doi.org/10.3103/S1068799810040148

    Medientyp :

    Aufsatz (Zeitschrift)

    Format :

    Elektronische Ressource

    Sprache :

    Englisch

    Schlagwörter :

    oval cylindrical shells , torsion , bending , internal pressure , nonlinear deformation , stability , finite element method Engineering , Automotive Engineering

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