Simple cumulative fatigue damage law used to estimate endurance of typical components when subjected to alternating wing loads encountered by aircraft in flight; study of damage in terms of infinitesimally small intervals of alternating load and corresponding fatigue strength; life of structure is governed almost entirely by gust velocity; results compared with criteria suggested by P.B.WALKER, and K. WALKER.


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    Titel :

    Estimation of fatigue damage in aircraft wing structures


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Chilver, A.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1954


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Methodologies for the Assessment of Widespread Fatigue Damage in Aircraft Wing Structures

    Collins, R. / Kimmins, S. / International Committee on Aeronautical Fatigue | British Library Conference Proceedings | 1999


    Modeling Projectile Damage in Transport Aircraft Wing Structures

    Hinrichsen, Ronald / Kurtz, Alex / Wang, John et al. | AIAA | 2006



    Modeling Projectile Damage in Transport Aircraft Wing Structures

    Hinrichsen, Ronald L. / Kurtz, Alex G. / Wang, John T. et al. | AIAA | 2008


    WING FOR AIRCRAFT DAMAGE

    TOLSTYJ ALEKSANDR SERGEEVICH / KHOKHANOV MIKHAIL ALEKSEEVICH / SHCHEPETEV DMITRIJ GENNADEVICH et al. | Europäisches Patentamt | 2019

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