2004
DOI: 10.1016/s1350-6307(03)00060-8
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Weight functions, CTOD, and related solutions for cracks at notches

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Cited by 52 publications
(40 citation statements)
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“…Other methods like weight function, Green's function, and collocation methods are also used to determine CTOD [15,16,17,18,19]. These methods may be complicated depending of the geometry and application, and have to be derived for a variety of geometries and loads.…”
Section: Introductionmentioning
confidence: 99%
“…Other methods like weight function, Green's function, and collocation methods are also used to determine CTOD [15,16,17,18,19]. These methods may be complicated depending of the geometry and application, and have to be derived for a variety of geometries and loads.…”
Section: Introductionmentioning
confidence: 99%
“…where, F σ is a "geometry evolution factor" and the stress intensity factor K I(Original) (a*, c*) is the value with original geometry (there no materials loss due to corrosion) obtained as per [15,16]. Here (a, c) and (a*, c*) denote the crack depths and surface crack lengths without an allowance for the loss of material due to corrosion and allowing for a reduction in the section thickness due to corrosion respectively.…”
Section: Failure Due To the Combined Action Of Corrosion And Fatiguementioning
confidence: 99%
“…Extract the stresses at the fatigue critical locations c) Use 3D, or 2D weight functions [14][15][16][17], or alternatively Trefftz function solutions [18 -20] to compute the K(a, c) solution space. Here "a" is the crack depth and "c" is the surface crack length.…”
Section: Introductionmentioning
confidence: 99%
“…The crack analysis method used here is based on a semi-analytical method proposed by Jones et al [9]. This semi-analytical method was used to compute the stress intensity factors associated with the cracks on the design (hole) surface.…”
Section: Residual Strength Evaluationmentioning
confidence: 99%
“…For each crack around the boundary, a set of gauss points are generated on the crack face, and the stresses at these points normal to the crack plane are computed. The stresses are then used to compute the stress intensity factors around the crack front using the FAST code (for details refer to [9]). For 3D cracks, the stress intensity factor varies along the crack fronts.…”
Section: Residual Strength Evaluationmentioning
confidence: 99%