Abstract Fatigue crack growth (FCG) analyses for metals and alloys properly began in the 1950s [1–6]. Test data [3–6] were obtained by optical measurements of the crack lengths visible on the specimen surfaces. In the same decade it was suspected [7] and demonstrated by optical fractography [8] that striations on fatigue fracture surfaces generally represented cycle-by-cycle progression of a crack.
Historical Review
Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components ; 1-20
2019-01-01
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Springer Verlag | 2023
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