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    The Radial-Equilibrium Equation of Turbomachinery

    Source: Journal of Engineering for Gas Turbines and Power:;1966:;volume( 088 ):;issue: 001::page 1
    Author:
    L. H. Smith
    DOI: 10.1115/1.3678471
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An equation is derived that describes the radial variation of circumferential-average flow properties inside of a turbomachine blade row. A physical interpretation is given for each of the several terms in the equation, and the magnitudes of the terms are demonstrated with an example. Annulus taper angle is found to be rather important. The error involved in the conventional axisymmetric (infinite-blade-number) approach is shown to be more related to the loading level, e.g., the lift-coefficient level, than the number of blades. This error is found to be small for the selected example.
    keyword(s): Equilibrium (Physics) , Equations , Turbomachinery , Blades , Errors , Flow (Dynamics) AND Annulus ,
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      The Radial-Equilibrium Equation of Turbomachinery

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    http://yetl.yabesh.ir/yetl1/handle/yetl/112724
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorL. H. Smith
    date accessioned2017-05-08T23:42:43Z
    date available2017-05-08T23:42:43Z
    date copyrightJanuary, 1966
    date issued1966
    identifier issn1528-8919
    identifier otherJETPEZ-26650#1_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112724
    description abstractAn equation is derived that describes the radial variation of circumferential-average flow properties inside of a turbomachine blade row. A physical interpretation is given for each of the several terms in the equation, and the magnitudes of the terms are demonstrated with an example. Annulus taper angle is found to be rather important. The error involved in the conventional axisymmetric (infinite-blade-number) approach is shown to be more related to the loading level, e.g., the lift-coefficient level, than the number of blades. This error is found to be small for the selected example.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Radial-Equilibrium Equation of Turbomachinery
    typeJournal Paper
    journal volume88
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3678471
    journal fristpage1
    journal lastpage12
    identifier eissn0742-4795
    keywordsEquilibrium (Physics)
    keywordsEquations
    keywordsTurbomachinery
    keywordsBlades
    keywordsErrors
    keywordsFlow (Dynamics) AND Annulus
    treeJournal of Engineering for Gas Turbines and Power:;1966:;volume( 088 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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