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    Increasing the Fatigue Strength of Loaded Holes by Dimpling

    Source: Journal of Engineering Materials and Technology:;1974:;volume( 096 ):;issue: 003::page 222
    Author:
    J. Shewchuk
    ,
    F. A. Roberts
    DOI: 10.1115/1.3443214
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new approach to improving the fatigue resistance of loaded holes in sheet material is presented. The material is first dimpled centering about the region where the hole is to be made, thus introducing tensile plastic strain. The dimple is then flattened and the hole drilled so that the region around the hole is under residual compressive stress. Zero to tension fatigue tests indicate considerable improvement in the fatigue strength of loaded holes as a result of dimpling. A fatigue strength improvement factor of nearly three for 106 cycles to failure was obtained based on the median lives of nominally 0.050-in. thick 2024-T3 aluminum alloy specimens.
    keyword(s): Fatigue strength , Fatigue testing , Sheet materials , Tension , Fatigue , Aluminum alloys , Electrical resistance , Compressive stress , Cycles AND Failure ,
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      Increasing the Fatigue Strength of Loaded Holes by Dimpling

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/164812
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    contributor authorJ. Shewchuk
    contributor authorF. A. Roberts
    date accessioned2017-05-09T01:38:13Z
    date available2017-05-09T01:38:13Z
    date copyrightJuly, 1974
    date issued1974
    identifier issn0094-4289
    identifier otherJEMTA8-26837#222_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164812
    description abstractA new approach to improving the fatigue resistance of loaded holes in sheet material is presented. The material is first dimpled centering about the region where the hole is to be made, thus introducing tensile plastic strain. The dimple is then flattened and the hole drilled so that the region around the hole is under residual compressive stress. Zero to tension fatigue tests indicate considerable improvement in the fatigue strength of loaded holes as a result of dimpling. A fatigue strength improvement factor of nearly three for 106 cycles to failure was obtained based on the median lives of nominally 0.050-in. thick 2024-T3 aluminum alloy specimens.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleIncreasing the Fatigue Strength of Loaded Holes by Dimpling
    typeJournal Paper
    journal volume96
    journal issue3
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.3443214
    journal fristpage222
    journal lastpage226
    identifier eissn1528-8889
    keywordsFatigue strength
    keywordsFatigue testing
    keywordsSheet materials
    keywordsTension
    keywordsFatigue
    keywordsAluminum alloys
    keywordsElectrical resistance
    keywordsCompressive stress
    keywordsCycles AND Failure
    treeJournal of Engineering Materials and Technology:;1974:;volume( 096 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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