The experiments are aimed to develop a new non-destructive method for fatigue damage diagnostics. This method is based on monitoring deformation roughness which is formed on the surface of aluminum structural alloys. The evolution of this roughness near the stress concentrator has been monitored at various stages of fatigue life under the stress level close to the operational stress level on the fuselage skin of modern aircraft. The deformation relief under static loads  is represented as well.


    Access

    Download


    Export, share and cite



    Title :

    DEFORMATION ROUGHNESS UNDER CYCLIC AND STATIC LOADS


    Contributors:


    Publication date :

    2005




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown





    Behavioural observation of laminated polymer composite under uniaxial quasi-static and cyclic loads

    Rafiquzzaman, M. / Abdullah, S. / Arifin, A. M. | British Library Online Contents | 2015


    Mathematical models of damage accumulation and crack resistance under static and cyclic loads

    Н.С. Кулик / А.Г. Кучер / В.Е. Мильцов | DOAJ | 2009

    Free access