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    Heat Transfer and Pumping on a Rotating Disk With Freely Induced and Forced Cooling

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 342
    Author:
    Darryl E. Metzger
    DOI: 10.1115/1.3445359
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of the heat transfer characteristics of flows between a high speed rotating disk and a parallel stationary shroud is presented. Flow and disk heat transfer rates have been determined for various combinations and rates of freely induced and forced flows supplied at both the hub and rim of the disk. The study models a practically important class of turbine rotor cooling problems where small flow rates similar in magnitude to the disk pumping flows are of interest. The experimental facility and procedures are described in detail. They have been designed to facilitate rapid and economical acquisition of rotor cooling characteristics in situations where the particular rotor-shroud geometry makes existing correlations inadequate.
    keyword(s): Heat transfer , Cooling , Rotating Disks , Flow (Dynamics) , Disks , Rotors , Turbines AND Geometry ,
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      Heat Transfer and Pumping on a Rotating Disk With Freely Induced and Forced Cooling

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142311
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorDarryl E. Metzger
    date accessioned2017-05-09T00:36:02Z
    date available2017-05-09T00:36:02Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#342_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142311
    description abstractAn experimental study of the heat transfer characteristics of flows between a high speed rotating disk and a parallel stationary shroud is presented. Flow and disk heat transfer rates have been determined for various combinations and rates of freely induced and forced flows supplied at both the hub and rim of the disk. The study models a practically important class of turbine rotor cooling problems where small flow rates similar in magnitude to the disk pumping flows are of interest. The experimental facility and procedures are described in detail. They have been designed to facilitate rapid and economical acquisition of rotor cooling characteristics in situations where the particular rotor-shroud geometry makes existing correlations inadequate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer and Pumping on a Rotating Disk With Freely Induced and Forced Cooling
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445359
    journal fristpage342
    journal lastpage348
    identifier eissn0742-4795
    keywordsHeat transfer
    keywordsCooling
    keywordsRotating Disks
    keywordsFlow (Dynamics)
    keywordsDisks
    keywordsRotors
    keywordsTurbines AND Geometry
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    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
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