In recent years, there has been a renewed interest in understanding the mechanical properties and microstructural characteristics of aluminum alloys containing lithium, because of their potential for extensive use in aerospace applications. In the present paper the fatigue crack propagation behavior of aluminum alloy 2020 (AlCuLiMnCd) in the peak strength temper is examined over a wide range of growth rates (from 10−6 to 10−11 m cycle−1). It was found that alloy 2020 shows crack propagation rates that are up to an order of magnitude slower at intermediate ΔK levels and up to two orders of magnitude slower in the near-threshold region, when compared with aluminum alloy 7075 under conditions of similar yield strength, load ratio, frequency and environment. Extensive analyses of the crack path for alloy 2020 reveal that pronounced deflection and branching of the fatigue crack occur at all growth rate levels as a result of a highly crystallographic mode of crack advance. The micromechanisms of fatigue crack growth in alloy 2020 are examined in terms of crack profile, fracture surface features, microstructure and environment.
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