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    Losses in Radial Inflow Turbines

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003::page 364
    Author:
    I. M. Khalil
    ,
    W. Tabakoff
    ,
    A. Hamed
    DOI: 10.1115/1.3448323
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A study was conducted to determine experimentally and theoretically the losses in radial inflow turbine nozzles. Extensive experimental data were obtained to investigate the flow behavior in a full-scale radial turbine stator annulus. A theoretical model to predict the losses in both the vaned and vaneless regions of the nozzle was developed. In this analysis, the interaction effects between the stator and the rotor are not considered. It was found that the losses incurred due to the end wall boundary layers can be significant, especially if they are characterized by a strong crossflow. The losses estimated using the analytical study are compared with the experimentally determined values.
    keyword(s): Turbines , Inflow , Stators , Nozzles , Rotors , Flow (Dynamics) , Boundary layers AND Annulus ,
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      Losses in Radial Inflow Turbines

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/88776
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    contributor authorI. M. Khalil
    contributor authorW. Tabakoff
    contributor authorA. Hamed
    date accessioned2017-05-08T23:00:56Z
    date available2017-05-08T23:00:56Z
    date copyrightSeptember, 1976
    date issued1976
    identifier issn0098-2202
    identifier otherJFEGA4-26897#364_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88776
    description abstractA study was conducted to determine experimentally and theoretically the losses in radial inflow turbine nozzles. Extensive experimental data were obtained to investigate the flow behavior in a full-scale radial turbine stator annulus. A theoretical model to predict the losses in both the vaned and vaneless regions of the nozzle was developed. In this analysis, the interaction effects between the stator and the rotor are not considered. It was found that the losses incurred due to the end wall boundary layers can be significant, especially if they are characterized by a strong crossflow. The losses estimated using the analytical study are compared with the experimentally determined values.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLosses in Radial Inflow Turbines
    typeJournal Paper
    journal volume98
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448323
    journal fristpage364
    journal lastpage371
    identifier eissn1528-901X
    keywordsTurbines
    keywordsInflow
    keywordsStators
    keywordsNozzles
    keywordsRotors
    keywordsFlow (Dynamics)
    keywordsBoundary layers AND Annulus
    treeJournal of Fluids Engineering:;1976:;volume( 098 ):;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
    yabeshDSpacePersian