STP982: A Comparison of Measurement Methods and Numerical Procedures for the Experimental Characterization of Fatigue Crack Closure

    Allison, JE
    Senior research scientist and research scientist, Ford Motor Company, Dearborn, MI

    Ku, RC
    Senior research scientist and research scientist, Ford Motor Company, Dearborn, MI

    Pompetzki, MA
    Graduate research assistant, University of Waterloo, Waterloo, Ontario

    Pages: 15    Published: Jan 1988


    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.

    Keywords:

    fatigue (materials), fatigue crack growth, crack closure, metals, alloys, titanium alloys, measurement techniques, crack-tip opening displacement


    Paper ID: STP27207S

    Committee/Subcommittee: E08.06

    DOI: 10.1520/STP27207S


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