A Comparison of Measurement Methods and Numerical Procedures for the Experimental Characterization of Fatigue Crack Closure

Abstract

Accurate experimental characterization of the crack closure process is important for a number of reasons, the most important of which may be for its use in developing materials and structures that are resistant to the growth of fatigue cracks. This paper describes the results of an investigation aimed at quantifying the point of crack closure. An α/β titanium alloy, Ti-6242S, was chosen for this investigation because its microstructure can be manipulated to produce large variations in the level of asperity-induced crack closure and is thus an ideal model alloy for understanding this important crack closure mechanism. Comparisons of two “global” compliance techniques (backface strain and crack mouth opening displacement) and a near crack-tip surface technique (two-stage replication) were made. In tests conducted at low stress intensities, all three methods gave nearly identical measurements of crack closure. For the two compliance techniques, different numerical procedures were used to determine the inflection point in the load-displacement curve. The magnitude of and variations in crack closure determined using these compliance methods were found to be strongly dependent on the numerical procedure used. Studies of crack-tip opening showed that in α/β-processed Ti-6242S the crack tip is tightly closed even at positive loads, indicating that plasticity induced closure is the predominant form of closure. In contrast, measurements in β-processed material showed that the crack tip is propped open even when no load is applied to the sample, indicating that closure in this microstructure is asperity-induced.

Evaluation of overload effects on fatigue crack growth and closure

“…From the load-displacement records, variations of the opening load, P op , were derived using the technique known as maximization of the correlation coefficient [31]. This technique involves taking the upper 10% of the P -e data and calculating the least squares correlation coefficient.…”

Influence of grain structure and slip planarity on fatigue crack growth in low alloying artificially aged 2xxx aluminium alloys

“…7. Though the difficulty in obtaining exact crack closure measurements is well reported [8,12,13,14], general trends in the sensitivity to crack closure of each alloy tested in the same condition can still be deduced. Fig.…”

Multi-scale crack closure measurements with digital image correlation on Haynes 230

“…The dependency of local crack opening levels on the distance from crack tip was investigated by considering three virtual extensometers placed at 50, 150 and 300 µm from the tip, as reported in Fig 6b, c and d. Crack opening was evaluated by fitting the portion of the COD vs ∆ plot in which the crack is fully open, as suggested in [14]. The opening load was defined as the stress level of the fitting line when the COD is equal to 0.…”