Abstract We developed a triangular discretization element of the fuselage fragment in the form of a thin shell compatible with the adjacent elements based on Lagrange multipliers. Solution of several test problems showed a high efficiency of using the modification of a triangular finite element being proposed.


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    Titel :

    Stress–strain analysis of a thin-shell part of fuselage using a triangular finite element with lagrange multipliers


    Beteiligte:
    Klochkov, Yu. V. (Autor:in) / Nikolaev, A. P. (Autor:in) / Vakhnina, O. V. (Autor:in) / Kiseleva, T. A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.07.2016


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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