1988
DOI: 10.21236/ada202636
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Three Dimensional Effects Near a Crack Tip in a Ductile Three Point Bend Specimen. Part 1. A Numerical Investigation

Abstract: A simultaneous numerical and experimental investigation is undertaken to assess three dimensional effects and HRR dominance near a crack front in a ductile 3-point bend specimen. In parallel to the 3-D numerical calculations, a plandIstrain and a plane-'stress analysis of the same in-plane specimen geometry is performed to obtain upper and lower bounds for the 3-D calculation. The radial, angular and thickness variation of the stresses and displacements are studied in great detail from contained yielding, to f… Show more

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Cited by 13 publications
(12 citation statements)
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“…This figure along with Figure 7, which shows that σ θ and σ h have very little thickness variation for r/ h > 0.5, suggest that plane stress conditions are approached for radial distances from the crack tip exceeding half the plate thickness. A similar observation was made for pure mode I loading by Narasimhan and Rosakis (1990) and Nakamura and Parks (1990).…”
Section: Radial Variation Of Stressessupporting
confidence: 79%
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“…This figure along with Figure 7, which shows that σ θ and σ h have very little thickness variation for r/ h > 0.5, suggest that plane stress conditions are approached for radial distances from the crack tip exceeding half the plate thickness. A similar observation was made for pure mode I loading by Narasimhan and Rosakis (1990) and Nakamura and Parks (1990).…”
Section: Radial Variation Of Stressessupporting
confidence: 79%
“…This disk is modeled using a finite element mesh comprised of eight-noded isoparametric hexahedral elements, which are focused at the crack tip (see Figure 1b). The crack front elements are formed by collapsing the eight-noded hexahedral elements to triangular prisms, while allowing for independent displacements of the nodes on the collapsed edge (as in Narasimhan and Rosakis, 1990).…”
Section: Modeling and Analysis Aspectsmentioning
confidence: 99%
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“…The layers of nodes are located at X 3 / h = 0.0, 0.038, 0.084, 0.14, 0.20, 0.28, 0.38, 0.5. Thus, the layers become gradually thinner as the free surface (X 3 = 0) is approached in order to capture the strong through-thickness variation of the field quantities close to the notch root (Narasimhan and Rosakis 1990;Subramanya et al 2007). …”
Section: Modeling Aspectsmentioning
confidence: 99%