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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2016-07-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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