The paper presents the results of research aimed at the fatigue evaluation of airframe elements made of aluminum alloys damaged by corrosion. Fatigue tests of the samples and metallographic studies were performed. The results of multi-year research on the effect of corrosion damage on the fatigue performance of aluminum alloys were summarized, and an observed dependence was established between the corrosion damage parameter and the material characteristics.


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    Title :

    Analytical-Experimental Evaluation of the Fatigue Resistance for Aircraft Fuselage Skin in the Case of Corrosion Damage


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 2 ; 181-188


    Publication date :

    2021-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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