YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Computation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004::page 881
    Author:
    Y. Nakata
    ,
    J. Y. Murthy
    ,
    D. E. Metzger
    DOI: 10.1115/1.2928043
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Convection heat transfer phenomena on rotating disks are of general interest in relation to turbomachineray design. In gas turbine engines, for example, knowledge of the temperature distribution on turbine disks that are bounded by a fluid cavity is required to predict stresses and durability. Cooling air is generally provided by the compressor section and routed to the turbine disk cavities where it is utilized for cooling both the rotating and stationary components. Since the production and pumping of the compressed cooling air imposes performance penalties on the engine cycle, a goal of the designer is always to minimize cooling air consumption. This requirement produces a need for accurate and detailed knowledge of the convection heat transfer and flow characteristics associated with disk cavity flows for a large variety of possible cooling configurations. In the past, most reliable information on disk cavity flow and heat transfer has been derived from empirical studies, but the large range of possible geometries and flow conditions precludes a complete coverage by experiment alone. In the future, it should be possible to supplement disk cavity flow experiments with numerical computations both to aid in interpretation of and to extend empirical results. The present numerical study of laminar flow cases is intended to complement previous experimental information for disk convection with jet impingment. The computational method is described and applied first to a baseline case of a rotating disk in an enclosure where results are found to compare favorably with the experiments of Daily and Nece. The two-dimensional approach used to model the inclusion of an impinging jet is described, and the computational method is applied to predict both flow and heat transfer characteristics in the vicinity of the interaction between impinging jet and rotating disk. The computed results partition into impingment-dominated and rotational-dominated regimes similar to the findings of prior experimental studies.
    keyword(s): Heat transfer , Laminar flow , Computation , Rotating Disks , Disks , Cooling , Cavity flows , Convection , Flow (Dynamics) , Turbines , Cavities , Computational methods , Temperature distribution , Cycles , Stress , Interior walls , Design , Durability , Gas turbines , Fluids , Engines AND Compressors ,
    • Download: (1.027Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Computation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/111053
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorY. Nakata
    contributor authorJ. Y. Murthy
    contributor authorD. E. Metzger
    date accessioned2017-05-08T23:39:50Z
    date available2017-05-08T23:39:50Z
    date copyrightOctober, 1992
    date issued1992
    identifier issn0889-504X
    identifier otherJOTUEI-28625#881_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111053
    description abstractConvection heat transfer phenomena on rotating disks are of general interest in relation to turbomachineray design. In gas turbine engines, for example, knowledge of the temperature distribution on turbine disks that are bounded by a fluid cavity is required to predict stresses and durability. Cooling air is generally provided by the compressor section and routed to the turbine disk cavities where it is utilized for cooling both the rotating and stationary components. Since the production and pumping of the compressed cooling air imposes performance penalties on the engine cycle, a goal of the designer is always to minimize cooling air consumption. This requirement produces a need for accurate and detailed knowledge of the convection heat transfer and flow characteristics associated with disk cavity flows for a large variety of possible cooling configurations. In the past, most reliable information on disk cavity flow and heat transfer has been derived from empirical studies, but the large range of possible geometries and flow conditions precludes a complete coverage by experiment alone. In the future, it should be possible to supplement disk cavity flow experiments with numerical computations both to aid in interpretation of and to extend empirical results. The present numerical study of laminar flow cases is intended to complement previous experimental information for disk convection with jet impingment. The computational method is described and applied first to a baseline case of a rotating disk in an enclosure where results are found to compare favorably with the experiments of Daily and Nece. The two-dimensional approach used to model the inclusion of an impinging jet is described, and the computational method is applied to predict both flow and heat transfer characteristics in the vicinity of the interaction between impinging jet and rotating disk. The computed results partition into impingment-dominated and rotational-dominated regimes similar to the findings of prior experimental studies.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComputation of Laminar Flow and Heat Transfer Over an Enclosed Rotating Disk With and Without Jet Impingement
    typeJournal Paper
    journal volume114
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2928043
    journal fristpage881
    journal lastpage890
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsLaminar flow
    keywordsComputation
    keywordsRotating Disks
    keywordsDisks
    keywordsCooling
    keywordsCavity flows
    keywordsConvection
    keywordsFlow (Dynamics)
    keywordsTurbines
    keywordsCavities
    keywordsComputational methods
    keywordsTemperature distribution
    keywordsCycles
    keywordsStress
    keywordsInterior walls
    keywordsDesign
    keywordsDurability
    keywordsGas turbines
    keywordsFluids
    keywordsEngines AND Compressors
    treeJournal of Turbomachinery:;1992:;volume( 114 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian