Abstract The possibility of estimating the fatigue life of aircraft structure at early stages of its design is considered. The assessment is performed based on a series of numerical experiments as well as the kinematic analysis and algorithms to search for rational parameters. The analysis is performed based on the finite element and superelement methods.


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    Titel :

    On the possibility of structural fatigue properties estimation at the early stages of design analysis


    Beteiligte:
    Kasumov, E. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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