Closure to “Mechanical Properties of First‐Year Sea Ice at Tarsiut Island” by Denis Blanchet, Razek Abdelnour, and George Comfort

Blanchet, Denis; Abdelnour, Razek; Comfort, G

doi:10.1061/(asce)0887-381x(1997)11:1(97)

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“…In addition, full-scale observations of ice-structure interactions suggest that while pure crushing is infrequent, fracture dominated events are more prevalent [ 1 ]. Global splitting or fracture of an ice feature has been proposed as a possible load limiting mechanism [2].…”

Section: Introductionmentioning

confidence: 99%

Fracture analysis of base-edge-cracked reverse-tapered plates

1995

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This paper presents a fracture mechanics analysis of the base-edge-cracked reverse-tapered (RT) fracture geometry. Motivation for this study was the use of this test geometry in Phase 1 of a recently completed jointindustry-agency project entitled 'Large-Scale Ice Fracture Experiments'. Underlying the choice of the RT fracture geometry for Phase 1 was the desirability of achieving crack propagation in a controlled and stable manner; such control would allow a number of observations to be made on one testpiece. Reverse tapering greatly improves not only crack growth stability but also crack path stability. The weight function method was used to provide accurate wide-ranging stress intensity factor (SIF), crack face displacement (COD) and crack opening area (COA) expressions for the RT subject to any loading. The required weight function was obtained through a finite element analysis of this geometry subject to a reference load case which determined the associated stress intensity factor and crack opening displacements. The Wu and Carlsson procedure was followed. A key modification to the latter procedure facilitated the attainment of the reference CMOD for all crack lengths, including the zero ligament limit; this was achieved by considering an additional reference solution. This modification is general in nature and could be pursued whenever the reference CMOD is not known analytically. An analytical solution for the crack opening area (COA) was also achieved for the special case of concentrated loading at the crack mouth. This solution can be applied to any geometry where the reference CMOD expression is known.

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Section: Introductionmentioning

confidence: 99%