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    Contact Stresses in Dovetail Attachments: Finite Element Modeling

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001::page 182
    Author:
    G. B. Sinclair
    ,
    N. G. Cormier
    ,
    J. H. Griffin
    ,
    G. Meda
    DOI: 10.1115/1.1391429
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The stress analysis of dovetail attachments presents some challenges. These challenges stem from the high stress gradients near the edges of contact and from the nonlinearities attending conforming contact with friction. To meet these challenges with a finite element analysis, refined grids are needed with mesh sizes near the edges of contact of the order of one percent of the local radii of curvature there. A submodeling procedure is described which can provide grids of sufficient resolution in return for moderate computational effort. This procedure furnishes peak stresses near contact edges which are converging on a sequence of three submodel grids, and which typically do converge to within about five percent.
    keyword(s): Stress , Finite element analysis AND Friction ,
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      Contact Stresses in Dovetail Attachments: Finite Element Modeling

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/126821
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorG. B. Sinclair
    contributor authorN. G. Cormier
    contributor authorJ. H. Griffin
    contributor authorG. Meda
    date accessioned2017-05-09T00:07:32Z
    date available2017-05-09T00:07:32Z
    date copyrightJanuary, 2002
    date issued2002
    identifier issn1528-8919
    identifier otherJETPEZ-26810#182_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126821
    description abstractThe stress analysis of dovetail attachments presents some challenges. These challenges stem from the high stress gradients near the edges of contact and from the nonlinearities attending conforming contact with friction. To meet these challenges with a finite element analysis, refined grids are needed with mesh sizes near the edges of contact of the order of one percent of the local radii of curvature there. A submodeling procedure is described which can provide grids of sufficient resolution in return for moderate computational effort. This procedure furnishes peak stresses near contact edges which are converging on a sequence of three submodel grids, and which typically do converge to within about five percent.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleContact Stresses in Dovetail Attachments: Finite Element Modeling
    typeJournal Paper
    journal volume124
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1391429
    journal fristpage182
    journal lastpage189
    identifier eissn0742-4795
    keywordsStress
    keywordsFinite element analysis AND Friction
    treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian