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    On the Theory of the Wells Turbine

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003::page 628
    Author:
    L. M. C. Gato
    ,
    A. F. de O. Falcão
    DOI: 10.1115/1.3239616
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A theoretical investigation is presented concerning the aerodynamic performance of the Wells turbine, a self-rectifying, axial-flow turbine suitable for energy extraction from a reciprocating air flow. A two-dimensional analysis is developed, and expressions, based on potential flow, are derived for the blade shape maximizing the turbine efficiency. Three-dimensional effects and profile losses are then accounted for by means of an actuator disk theory, which shows that large radial distortions of axial velocity profile can occur, depending on blade shape, with important implications on the extent of the stall-free conditions.
    keyword(s): Wells , Turbines , Blades , Shapes , Flow (Dynamics) , Disks , Axial flow , Air flow AND Actuators ,
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      On the Theory of the Wells Turbine

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/98406
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorL. M. C. Gato
    contributor authorA. F. de O. Falcão
    date accessioned2017-05-08T23:17:46Z
    date available2017-05-08T23:17:46Z
    date copyrightJuly, 1984
    date issued1984
    identifier issn1528-8919
    identifier otherJETPEZ-26607#628_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/98406
    description abstractA theoretical investigation is presented concerning the aerodynamic performance of the Wells turbine, a self-rectifying, axial-flow turbine suitable for energy extraction from a reciprocating air flow. A two-dimensional analysis is developed, and expressions, based on potential flow, are derived for the blade shape maximizing the turbine efficiency. Three-dimensional effects and profile losses are then accounted for by means of an actuator disk theory, which shows that large radial distortions of axial velocity profile can occur, depending on blade shape, with important implications on the extent of the stall-free conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Theory of the Wells Turbine
    typeJournal Paper
    journal volume106
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239616
    journal fristpage628
    journal lastpage633
    identifier eissn0742-4795
    keywordsWells
    keywordsTurbines
    keywordsBlades
    keywordsShapes
    keywordsFlow (Dynamics)
    keywordsDisks
    keywordsAxial flow
    keywordsAir flow AND Actuators
    treeJournal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 003
    contenttypeFulltext
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