The free vibration analysis of laminated composite cylindrical, spherical, hypar, saddle, and elliptical shells with cutouts and concentrated mass is presented by developing a C 0 finite element formulation based on third-order shear deformation theory (TSDT). The proposed model satisfies the zero transverse shear stress conditions at shell top and bottom without using a shear correction factor. This is the first finite element implementation of the TSDT to solve the vibration problem of laminated composite shells with cutouts and concentrated mass incorporating cross curvature effects in shells. Parametric vibration study has been performed for different shells with cutouts and concentrated mass.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Vibration of Laminated Composite Shells with Cutouts and Concentrated Mass


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 56 , 4 ; 1662-1678


    Erscheinungsdatum :

    2017-11-16


    Format / Umfang :

    17 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Optimally Reinforced Cutouts in Laminated Circular Cylindrical Shells

    Senocak, E. / Waas, A. / American Institute of Aeronautics and Astronautics| ASME| ASCE | British Library Conference Proceedings | 1995



    Buckling of Composite Cylindrical Shells with Circular Cutouts

    Schiller, Arne / Bisagni, Chiara | AIAA | 2022