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    Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003::page 264
    Author:
    A. Yamamoto
    DOI: 10.1115/1.3262265
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the mechanisms of three-dimensional flows and of the associated losses occurring near the tip endwall region of a linear turbine cascade with tip clearance. The clearance gap sizes and the cascade incidences were chosen as the most important variables affecting the mechanisms. Flows close to the endwall and inside the clearance were surveyed in great detail using a micro five-hole pitot tube of 0.6 mm head size. The results gave very detailed information on the mechanisms, such as leakage flow vectors and pressure distributions throughout the clearance. Interaction of leakage flow with the endwall flow and their associated separation lines, effects of gap size and inlet flow angle on loss generation, and skewness of the three-dimensional endwall flows are also discussed.
    keyword(s): Cascades (Fluid dynamics) , Clearances (Engineering) , Turbines , Blades , Flow (Dynamics) , Mechanisms , Leakage flows , Pressure , Separation (Technology) AND Flowmeters ,
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      Endwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance

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    http://yetl.yabesh.ir/yetl1/handle/yetl/106161
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    contributor authorA. Yamamoto
    date accessioned2017-05-08T23:31:20Z
    date available2017-05-08T23:31:20Z
    date copyrightJuly, 1989
    date issued1989
    identifier issn0889-504X
    identifier otherJOTUEI-28596#264_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106161
    description abstractThis paper discusses the mechanisms of three-dimensional flows and of the associated losses occurring near the tip endwall region of a linear turbine cascade with tip clearance. The clearance gap sizes and the cascade incidences were chosen as the most important variables affecting the mechanisms. Flows close to the endwall and inside the clearance were surveyed in great detail using a micro five-hole pitot tube of 0.6 mm head size. The results gave very detailed information on the mechanisms, such as leakage flow vectors and pressure distributions throughout the clearance. Interaction of leakage flow with the endwall flow and their associated separation lines, effects of gap size and inlet flow angle on loss generation, and skewness of the three-dimensional endwall flows are also discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEndwall Flow/Loss Mechanisms in a Linear Turbine Cascade With Blade Tip Clearance
    typeJournal Paper
    journal volume111
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262265
    journal fristpage264
    journal lastpage275
    identifier eissn1528-8900
    keywordsCascades (Fluid dynamics)
    keywordsClearances (Engineering)
    keywordsTurbines
    keywordsBlades
    keywordsFlow (Dynamics)
    keywordsMechanisms
    keywordsLeakage flows
    keywordsPressure
    keywordsSeparation (Technology) AND Flowmeters
    treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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