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- W4313888843 abstract "Fatigue crack grows faster in the integral structure than in the riveted structures. This study compares the bonded, cold-sprayed and ultrasonically consolidated crack retarders to increase the fatigue life of integral airframe structure. The 2024-T351 aluminum M(T) specimen reinforced with crack retarders made of AISI 301 and 316L steels, Ti-6Al-4V titanium alloy and unidirectional CFRP laminate are evaluated in terms of fatigue life, delamination resistance and weight efficiency. Specimens were subjected to constant amplitude loading up to the final failure. A substantial decrease in fatigue crack growth rate was achieved using the ultrasonically consolidated AISI 301 crack retarder." @default.
- W4313888843 created "2023-01-10" @default.
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- W4313888843 date "2023-05-01" @default.
- W4313888843 modified "2023-10-18" @default.
- W4313888843 title "Bonded and additively manufactured crack retarders: A comparative study of damage tolerance properties" @default.
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- W4313888843 doi "https://doi.org/10.1016/j.ijfatigue.2023.107509" @default.
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