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    Residual Stress Measurement and Fatigue Crack Growth Prediction after Cold Expansion of Cracked Fastener Holes

    Source: Journal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003
    Author:
    D. Stefanescu
    ,
    J. R. Santisteban
    ,
    L. Edwards
    ,
    M. E. Fitzpatrick
    DOI: 10.1061/(ASCE)0893-1321(2004)17:3(91)
    Publisher: American Society of Civil Engineers
    Abstract: The cold expansion technique is often used to introduce beneficial compressive stress at fastener holes, and can be used for remedial work where cracks already exist. In this paper, results are presented showing the effect of preexisting cracks on the residual stress field produced by cold expanding a fastener hole, and on subsequent fatigue crack growth. The effect on the residual stresses was experimentally evaluated in two ways: indirectly, in terms of retained expansion and directly, by measurement of the stresses using the X-ray and neutron diffraction techniques. The retained expansion ratio showed that cold expansion is more sensitive to the existence of precracks at lower levels of applied interference, and the inlet and outlet faces have different behavior. The stress measurements showed that preexisting cracks reduce the compressive residual stresses more on the mandrel inlet face than on the outlet face and in the middle of the specimen. The effect on fatigue crack growth rates was modeled using a linear-elastic fracture mechanics approach. It was found that cold expansion of a hole containing a preexisting crack longer than 1 mm introduces little benefit for subsequent fatigue crack growth behavior.
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      Residual Stress Measurement and Fatigue Crack Growth Prediction after Cold Expansion of Cracked Fastener Holes

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    http://yetl.yabesh.ir/yetl1/handle/yetl/45007
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    • Journal of Aerospace Engineering

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    contributor authorD. Stefanescu
    contributor authorJ. R. Santisteban
    contributor authorL. Edwards
    contributor authorM. E. Fitzpatrick
    date accessioned2017-05-08T21:16:10Z
    date available2017-05-08T21:16:10Z
    date copyrightJuly 2004
    date issued2004
    identifier other%28asce%290893-1321%282004%2917%3A3%2891%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45007
    description abstractThe cold expansion technique is often used to introduce beneficial compressive stress at fastener holes, and can be used for remedial work where cracks already exist. In this paper, results are presented showing the effect of preexisting cracks on the residual stress field produced by cold expanding a fastener hole, and on subsequent fatigue crack growth. The effect on the residual stresses was experimentally evaluated in two ways: indirectly, in terms of retained expansion and directly, by measurement of the stresses using the X-ray and neutron diffraction techniques. The retained expansion ratio showed that cold expansion is more sensitive to the existence of precracks at lower levels of applied interference, and the inlet and outlet faces have different behavior. The stress measurements showed that preexisting cracks reduce the compressive residual stresses more on the mandrel inlet face than on the outlet face and in the middle of the specimen. The effect on fatigue crack growth rates was modeled using a linear-elastic fracture mechanics approach. It was found that cold expansion of a hole containing a preexisting crack longer than 1 mm introduces little benefit for subsequent fatigue crack growth behavior.
    publisherAmerican Society of Civil Engineers
    titleResidual Stress Measurement and Fatigue Crack Growth Prediction after Cold Expansion of Cracked Fastener Holes
    typeJournal Paper
    journal volume17
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2004)17:3(91)
    treeJournal of Aerospace Engineering:;2004:;Volume ( 017 ):;issue: 003
    contenttypeFulltext
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