147 research outputs found

    Different aspects of low-cycle fatigue

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    The experimental and theoretical knowledge in this field is presented. The different relations which correlate the number of cyles to rupture with strain or strain-energy are given. The application of low-cycle fatigue concepts to the crack initiation and crack propagation are briefly studied

    Can acoustic emission detect the initiation of fatigue cracks: Application to high-strength light alloys used in aeronautics

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    Acoustic emission was used for the detection of fatigue cracking in a number of high-strength light alloys used in aeronautical structures. Among the features studied were: the influence of emission frequency, the effect of surface oxidation, and the influence of grains. It was concluded that acoustic emission is an effective nondestructive technique for evaluating the initiation of fatigue cracking in such materials

    Pinning/depinning of crack fronts in heterogeneous materials

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    The fatigue fracture surfaces of a metallic alloy, and the stress corrosion fracture surfaces of glass are investigated as a function of crack velocity. It is shown that in both cases, there are two fracture regimes, which have a well defined self-affine signature. At high enough length scales, the universal roughness index 0.78 is recovered. At smaller length scales, the roughness exponent is close to 0.50. The crossover length ξc\xi_c separating these two regimes strongly depends on the material, and exhibits a power-law decrease with the measured crack velocity ξcvϕ\xi_c \propto v^{-\phi}, with ϕ1\phi \simeq 1. The exponents ν\nu and β\beta characterising the dependence of ξc\xi_c and vv upon the pulling force are shown to be close to ν2\nu \simeq 2 and β2\beta \simeq 2.Comment: 4 pages, latex, and 4 encapsulated postscript figure
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