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.
Analytical-Experimental Evaluation of the Fatigue Resistance for Aircraft Fuselage Skin in the Case of Corrosion Damage
Russ. Aeronaut.
Russian Aeronautics ; 64 , 2 ; 181-188
2021-04-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
British Library Online Contents | 1994
|British Library Conference Proceedings | 1994
|Experimental techniques for aircraft fuselage structures containing damage
British Library Conference Proceedings | 2004
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