The theoretical foundations of fatigue crack growth kinetics in aircraft structures are presented. The influence of different cycles and modes of loading on crack growth rate is investigated. Modeling of the fatigue cracks propagation is carried out taking into account many factors. A semiphenomenological model of fatigue crack growth kinetics prediction is considered and refined, the possibility of its application to aircraft structures is shown.


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    Title :

    Features of prediction of fatigue crack propagation kinetics in aircraft structures



    Conference:

    XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION ; 2021 ; Moscow, Russia


    Published in:

    Publication date :

    2023-07-20


    Size :

    6 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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