1991
DOI: 10.1016/0921-5093(91)90688-j
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Fatigue damage accumulation in nickel prior to crack initiation

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Cited by 34 publications
(35 citation statements)
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“…From the data of Grobstein et al (1991) for uniaxial, fully reversed, stress-controlled loading at 154MPa, we obtain A ≈ 8.6 x 10 -10 MPa -3 m -0.5 cycle -1 assuming from the data that ∆N ≈ 3.3 x 10 3 cycles, N total ≈ 2.23 x 10 4 cycles, and C crk ≈ 10 7 m -3 (Nazarov and Sutin 1963).…”
Section: Polycrystalline Nickel Nonlinearity Parameter Versus Percentmentioning
confidence: 99%
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“…From the data of Grobstein et al (1991) for uniaxial, fully reversed, stress-controlled loading at 154MPa, we obtain A ≈ 8.6 x 10 -10 MPa -3 m -0.5 cycle -1 assuming from the data that ∆N ≈ 3.3 x 10 3 cycles, N total ≈ 2.23 x 10 4 cycles, and C crk ≈ 10 7 m -3 (Nazarov and Sutin 1963).…”
Section: Polycrystalline Nickel Nonlinearity Parameter Versus Percentmentioning
confidence: 99%
“…It is these basic building blocks that determine the magnitude of the nonlinearity parameters. In this view we naively assume that since AA2024-T4 is also a wavy slip metal, the nonlinearity parameters of the alloy may be obtained from the substructural evolution data of nickel Grobstein et al (1991) and the elastic constants, Poisson ratio, and Burgers vector for AA2024-T4.…”
Section: Dependence Of Nonlinearity Parameters Of Nickel and Aa2024-tmentioning
confidence: 99%
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