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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    2014-01-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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