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Partial crack closure under block loading [PDF]
Fatigue crack propagation tests under high-low and low-high block loading sequences have been performed in aluminium alloy specimens. The tests were carried out at constant [Delta]K conditions. Two stress ratios were analysed: R = 0.05 and R = 0.4. Crack
L P Borrego, J M Ferreira, J D Costa
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Effect of crack closure on crack initiation parameters
Engineering Fracture Mechanics, 1986Young’s modulus shear modulus elastic constant : 3 -4y plane strain ; 3 -r/l + y plane stress force per unit thickness of plate open end mode I stress intensity factor open end mode II stress intensity factor Poisson’s ratio applied uniform tension, 2p/k + 1 distance of concentrated force from centre line of crack maximum normal stress minimum strain ...
R.S. Alwar, S. Thiagarajan
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Fatigue crack closure for inclined and kinked cracks
International Journal of Fracture, 2002This paper presents recent work on finite element modelling of plasticity-induced fatigue crack closure occurring in cracks which are inclined to the loading axis, and which may then develop a kink. Such crack deviations occur naturally during crack growth, and improved life prediction models require understanding of the effects of such inclined ...
L.-W. Wei, M.N. James
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Analysis of crack-dislocation interaction: crack closure, crack opening
Materials Science and Engineering: A, 1994Abstract The decrease in stress intensity factor, expected from dislocation emission at a crack tip, can be achieved either through a change in crack tip radius (blunting) or through a crack closure induced by the dislocation (shielding) opposite to the opening imposed by the external stress field.
M.A. Loyola de Oliveira, G. Michot
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Crack growth and closure behaviour of surface cracks
International Journal of Fatigue, 2004Abstract This paper investigated the crack growth and closure behaviour of surface cracks in AISI 4130 alloy steel under the constant amplitude loading and single-overload conditions. The compliance measurements of depth- and surface-wise crack closure were performed using the backface strain gauge and the near-tip gauge, respectively.
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Some experimental observations on crack closure and crack‐tip plasticity
Fatigue & Fracture of Engineering Materials & Structures, 2009ABSTRACTThis study presents a methodology for evaluating crack closure and the effect of crack‐tip plasticity on stress intensity. Full‐field displacement maps obtained by digital image correlation are used to obtain the mixed‐mode, crack‐driving force.
Lopez-Crespo, P +4 more
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Modelling Crack Closure for an Interface Crack Under Harmonic Loading
International Journal of Fracture, 2010zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Menshykova, Maryna V. +2 more
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Characterization of Crack Closure
1985Crack opening and closure levels are determined for small cracks growing from sharp and blunt notches during cyclic loading. Crack tip opening displacement measurements as low as 0.1 μm are reported. Experimental crack opening levels are compared with analytical crack opening levels for various stress intensity ranges, crack lengths, and R-ratios.
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1984
Abstract : A comprehensive review and critique of the literature on fatigue crack closure is presented. The elements of closure; its mechanisms, experimental procedures for its determination; the phenomenological study of its dependence on different variables, and methodologies for its prediction, are all discussed in detail.
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Abstract : A comprehensive review and critique of the literature on fatigue crack closure is presented. The elements of closure; its mechanisms, experimental procedures for its determination; the phenomenological study of its dependence on different variables, and methodologies for its prediction, are all discussed in detail.
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On the geometry of fatigue crack closure
Steel Research, 1992Long fatigue cracks frequently grow at a much lower rate than short cracks because they are closed during part of the stress cycle. The critical crack length for the transition from “short” to “long” depends on the amplitude of stress intensity ΔK and on the stress ratio R. This dependence is explained using a numerical study of the crack flank contour.
Hein‐Peter Stüwe +2 more
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