Abstract A technique for choosing a rational load-carrying scheme and weight analysis at the early stages of designing lifting surfaces with the use of a special model of the finite element method is proposed. The distribution of structure loads is determined with regard for its deformation. The numerical example is presented.


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    Titel :

    Structural optimization of lifting surfaces with regard to static aeroelasticity


    Beteiligte:
    Boldyrev, A. V. (Autor:in) / Komarov, V. A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2008-06-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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