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    Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003::page 375
    Author:
    A. Yamamoto
    ,
    Y. Kondo
    ,
    R. Murao
    DOI: 10.1115/1.2927886
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to understand overall performance and internal flows of air-cooled turbine blade rows, flows in a model linear cascade were surveyed with secondary air injection from various locations of the blade surfaces. The secondary air interacted with the cascade passage vortices and changed the loss distribution significantly. The cascade overall loss decreased when the air was injected along the mainstream and increased when the air was injected against the mainstream from some locations of the blade leading edge. Effects on overall kinetic energy of the secondary flows and on the cascade outlet flow angle were also discussed in this paper.
    keyword(s): Flow (Dynamics) , Cooling , Cascades (Fluid dynamics) , Turbines , Blades , Vortices , Internal flow , Kinetic energy AND Turbine blades ,
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      Cooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109377
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    contributor authorA. Yamamoto
    contributor authorY. Kondo
    contributor authorR. Murao
    date accessioned2017-05-08T23:36:55Z
    date available2017-05-08T23:36:55Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28613#375_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109377
    description abstractIn order to understand overall performance and internal flows of air-cooled turbine blade rows, flows in a model linear cascade were surveyed with secondary air injection from various locations of the blade surfaces. The secondary air interacted with the cascade passage vortices and changed the loss distribution significantly. The cascade overall loss decreased when the air was injected along the mainstream and increased when the air was injected against the mainstream from some locations of the blade leading edge. Effects on overall kinetic energy of the secondary flows and on the cascade outlet flow angle were also discussed in this paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCooling-Air Injection Into Secondary Flow and Loss Fields Within a Linear Turbine Cascade
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927886
    journal fristpage375
    journal lastpage383
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsCooling
    keywordsCascades (Fluid dynamics)
    keywordsTurbines
    keywordsBlades
    keywordsVortices
    keywordsInternal flow
    keywordsKinetic energy AND Turbine blades
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;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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