Abstract

New experimental technique for a determination of the stress intensity factor (SIF) and T-stress values is developed and verified. The approach assumes combining the crack compliance method and optical interferometric measurements of local deformation response on small crack length increment. Initial experimental information has a form of in-plane displacement component values, which are measured byelectronic speckle-pattern interferometry at some specific points located near a crack tip. Required values offracture mechanics parameters follow from the first four coefficients of Williams’ series. A determination ofinitial experimental data at the nearest vicinity of notch tip is the main feature of the developed approach. Thatis why it is not necessary to involve complex numerical models, which include global geometrical parameters,loading and boundary conditions of the object under study, in a stage of experimental data interpretation. Anavailability of high-quality interference fringe patterns, which are free from rigid-body motions, serves as areliable indicator of real stress state around a crack tip. A verification of the technique is performed bycomparing experimental results with analogous data of FEM modelling. Experimentally determined mode I SIFfor DCB specimen with end crack is in 5 per cent agreement with the numerically simulated case. Proposedapproach is capable of estimating an influence of the notch radius on fracture mechanics parameters.Comparing SIF and T-stress obtained for U-notches of different radius both in actual and residual stress fieldconfirms this statement.

Highlights

  • Experimental determination of stress intensity factor (SIF) and T-stress for a crack of constant length under external load increment is of considerable current interest [1,2,3,4,5,6,7,8]

  • This presentation is devoted to a development and verification of new technique for a determination of SIF and T-stress values by combining the crack compliance method and optical interferometric measurements of local deformation response on small crack length increment

  • M odified version of the crack compliance method resides in recording interference fringe patterns, which correspond to a difference between two in-plane displacement component fields

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Summary

Introduction

Experimental determination of stress intensity factor (SIF) and T-stress for a crack of constant length under external load increment is of considerable current interest [1,2,3,4,5,6,7,8]. M odified version of the crack compliance method resides in recording interference fringe patterns, which correspond to a difference between two in-plane displacement component fields.

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